diff --git a/.gitignore b/.gitignore
index 89988e792434ebd924eb04146d7dc526fca8a333..adc07191da96ad6c2171452348da6ada8beebf46 100644
--- a/.gitignore
+++ b/.gitignore
@@ -3,7 +3,6 @@
 *.o
 obj/
 *.res
-projects/
 
 # IDE Files
 .vscode
diff --git a/projects/newFormat-CSMR-2020.xml b/projects/newFormat-CSMR-2020.xml
new file mode 100644
index 0000000000000000000000000000000000000000..925455677c2ec5c63db49b40a49280c4566277ae
--- /dev/null
+++ b/projects/newFormat-CSMR-2020.xml
@@ -0,0 +1,10198 @@
+<aircraft_exchange_file>
+    <requirements_and_specifications description="Requirements and specifications">
+        <general description="General aircraft information">
+            <type description="Aircraft type">
+                <value>CeRAS</value>
+            </type>
+            <model description="Model - Version">
+                <value>SMR-2020</value>
+            </model>
+        </general>
+        <mission_files description="Name of xml files which are located in the missionData directory and contain the flight phase data" tool_level="0">
+            <design_mission_file description="Name of the design mission xml">
+                <value>design_mission.xml</value>
+            </design_mission_file>
+            <study_mission_file description="Name of the study mission xml">
+                <value>study_mission.xml</value>
+            </study_mission_file>
+            <requirements_mission_file description="Name of the  requirements mission xml">
+                <value>requirements_mission.xml</value>
+            </requirements_mission_file>
+        </mission_files>
+        <design_specification description="Design specification">
+            <configuration description="Configuration information">
+                <aerodynamic_technologies description="Integration of aerodynamic technologies on the aircraft: true / false">
+                    <value>false</value>
+                </aerodynamic_technologies>
+                <configuration_type description="aircraft configuration: tube_and_wing / blended_wing_body">
+                    <value>tube_and_wing</value>
+                </configuration_type>
+                <fuselage_definition description="Design description of the fuselage.">
+                    <fuselage_type description="Fuselage type: single_aisle / wide_body">
+                        <value>single_aisle</value>
+                    </fuselage_type>
+                    <fuselage_pressurization description="Switch to select a pressurized fuselage. (true: pressurized fuselage, false: non pressurized fuselage)">
+                        <value>true</value>
+                    </fuselage_pressurization>
+                    <blended_wing_body_configuration description="Additional design description for blended wing body configurations.">
+                        <number_of_payload_tubes description="Number of fuselage tubes for blendend wing body configurations. For tube and wing configuration is set to 1.">
+                            <value>1</value>
+                            <unit>1</unit>
+                            <default>1</default>
+                            <lower_boundary>1</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </number_of_payload_tubes>
+                        <center_body_wing_sweep description="Sweep of the leading edge of the center body.">
+                            <value>60</value>
+                            <unit>degree</unit>
+                            <default>60</default>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>75</upper_boundary>
+                            <center_body_wing_sweep_tolerance Desc="Permissible deviation of the actual from the desired leading edge sweep of the center body.">
+                                <value>5</value>
+                                <unit>degree</unit>
+                                <default>5</default>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15</upper_boundary>
+                            </center_body_wing_sweep_tolerance>
+                        </center_body_wing_sweep>
+                    </blended_wing_body_configuration>
+                </fuselage_definition>
+                <wing_definition description="Definitions for wing design">
+                    <mounting description="wing mounting for tube_and_wing configuration (ignored at blended_wing_body) - low / mid / high">
+                        <value>low</value>
+                    </mounting>
+                </wing_definition>
+                <empennage_definition description="Definitions for empennage design">
+                    <empennage_type description="tube_and_wing configuration: conventional - blended_wing_body: vertical_tails">
+                        <value>conventional</value>
+                    </empennage_type>
+                </empennage_definition>
+                <undercarriage_definition description="Design description of the undercarriage.">
+                    <main_gear_mounting description="Mounting position of the main landing gear: wing_mounted / fuselage_mounted.">
+                        <value>wing_mounted</value>
+                    </main_gear_mounting>
+                    <undercarriage_retractability description="Switch to set retractability of landing gear: retractable / non_retractable.">
+                        <value>retractable</value>
+                    </undercarriage_retractability>
+                </undercarriage_definition>
+                <tank_definition description="Energy tanks information">
+                    <tank ID="0" description="Inner left tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+                            <value>inner_left</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="1" description="Outer left tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+                            <value>outer_left</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="2" description="Inner right tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+                            <value>inner_right</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="3" description="Outer right tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+                            <value>outer_right</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="4" description="Center wing tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>wing</value>
+                        </location>
+                        <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+                            <value>center</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="5" description="Additional center tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>fuselage</value>
+                        </location>
+                        <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+                            <value>center</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                    <tank ID="6" description="Trim tank">
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                        <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer">
+                            <value>horizontal_stabilizer</value>
+                        </location>
+                        <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total">
+                            <value>total</value>
+                        </position>
+                        <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks.">
+                            <value>0.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>1.0</upper_boundary>
+                        </energy_share>
+                    </tank>
+                </tank_definition>
+                <loads description="Loads information">
+                    <design_load_factor description="design load factor n">
+                        <maximum description="maximum design load factor n">
+                            <value>2.5</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>4</upper_boundary>
+                        </maximum>
+                        <minimum description="maximum design load factor n">
+                            <value>-1.0</value>
+                            <unit>1</unit>
+                            <lower_boundary>-2.0</lower_boundary>
+                            <upper_boundary>0.0</upper_boundary>
+                        </minimum>
+                        <maneuver description="standard maneuver load factor for e.g. flare">
+                            <value>1.1</value>
+                            <unit>1</unit>
+                            <lower_boundary>0.0</lower_boundary>
+                            <upper_boundary>2.0</upper_boundary>
+                        </maneuver>
+                    </design_load_factor>
+                </loads>
+            </configuration>
+            <transport_task description="Define the transport task for aircraft project.">
+                <passenger_definition description="Define the masses of the passengers">
+                    <total_number_passengers description="Design number of passengers">
+                        <value>180</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1000</upper_boundary>
+                    </total_number_passengers>
+                    <mass_per_passenger description="Design mass of a single passenger WITHOUT luggage">
+                        <value>80</value>
+                        <unit>kg</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>200</upper_boundary>
+                    </mass_per_passenger>
+                    <luggage_mass_per_passenger description="Design mass of a the luggage for a single passenger">
+                        <value>15</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>25</upper_boundary>
+                    </luggage_mass_per_passenger>
+                </passenger_definition>
+                <multi_passenger_deck_layout description="Switch to select a multi passenger deck fuselage design. (true: multi passenger deck allowed, false: multi passenger deck denied)">
+                    <value>false</value>
+                    <default>false</default>
+                    <specific_number_of_passenger_decks>
+                        <value>2</value>
+                        <unit>-</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>3</upper_boundary>
+                        <default>2</default>
+                    </specific_number_of_passenger_decks>
+                </multi_passenger_deck_layout>
+                <passenger_class_definition>
+                    <class_distribution description="Relative passenger distribution for the classes: President Class/First Class/Business Class/Premium Economy/Economy. Sum must be equal to 1!">
+                        <value>0/0/0/0/1</value>
+                    </class_distribution>
+                </passenger_class_definition>
+                <cargo_definition description="Definition of cargo which does not belong to passengers">
+                    <additional_cargo_mass description="Mass of cargo which does not belong to passengers">
+                        <value>2200</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>25000</upper_boundary>
+                    </additional_cargo_mass>
+                    <cargo_density description="Density of cargo which does not belong to passengers">
+                        <value>165</value>
+                        <unit>kg/m^3</unit>
+                        <lower_boundary>150</lower_boundary>
+                        <upper_boundary>200</upper_boundary>
+                    </cargo_density>
+                </cargo_definition>
+            </transport_task>
+            <energy_carriers description="Energy carriers information">
+                <energy_carrier ID="0" description="One specific energy carrier">
+                    <type description="Energy type (for multifuel engine create new ID). Selector: kerosene / liquid_hydrogen / battery / saf">
+                        <value>kerosene</value>
+                    </type>
+                    <density description="Energy carrier density.">
+                        <value>785</value>
+                        <unit>kg/m^3</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>10000</upper_boundary>
+                    </density>
+                    <volumetric_density description="Volumetric energy density of energy carrier.">
+                        <value>33.833</value>
+                        <unit>J/m^3</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1e+12</upper_boundary>
+                    </volumetric_density>
+                    <gravimetric_density description="Gravimetric energy density of energy carrier.">
+                        <value>43100000</value>
+                        <unit>J/kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1e+12</upper_boundary>
+                    </gravimetric_density>
+                </energy_carrier>
+            </energy_carriers>
+            <propulsion description="Propulsion information">
+                <propulsor ID="123" description="Information for specific propulsor">
+                    <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell">
+                        <value>turbo</value>
+                    </powertrain>
+                    <type description="Type of main thrust generator. Selector: fan / prop">
+                        <value>fan</value>
+                    </type>
+                    <position description="propulsor position (arrangement order acc to ID order)">
+                        <parent_component description="position on component. Selector: wing / fuselage / empennage">
+                            <value>wing</value>
+                        </parent_component>
+                        <x description="x-position (aircraft coordinate system). Selector: front / back">
+                            <value>front</value>
+                        </x>
+                        <y description="y position (aircraft coordinate system). Selector: left / right">
+                            <value>left</value>
+                        </y>
+                        <z description="z position (aircraft coordinate system). Selector: over / mid / under / in">
+                            <value>under</value>
+                        </z>
+                    </position>
+                    <energy_carrier_ID description="see energy carrier specification node">
+                        <value>999</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </energy_carrier_ID>
+                    <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+                        <value>0.5</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </thrust_share>
+                </propulsor>
+                <propulsor ID="1" description="Information for specific propulsor">
+                    <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell">
+                        <value>turbo</value>
+                    </powertrain>
+                    <type description="Type of main thrust generator. Selector: fan / prop">
+                        <value>fan</value>
+                    </type>
+                    <position description="propulsor position (arrangement order acc to ID order)">
+                        <parent_component description="position on component. Selector: wing / fuselage / empennage">
+                            <value>wing</value>
+                        </parent_component>
+                        <x description="x-position (aircraft coordinate system). Selector: front / back">
+                            <value>front</value>
+                        </x>
+                        <y description="y position (aircraft coordinate system). Selector: left / right">
+                            <value>right</value>
+                        </y>
+                        <z description="z position (aircraft coordinate system). Selector: over / mid / under / in">
+                            <value>under</value>
+                        </z>
+                    </position>
+                    <energy_carrier_ID description="see energy carrier specification node">
+                        <value>888</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </energy_carrier_ID>
+                    <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+                        <value>0.5</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </thrust_share>
+                </propulsor>
+                <propulsor ID="10" description="Information for specific propulsor">
+                    <powertrain description="Way the power is generated from the source. Selector: turbo / electric / fuel_cell">
+                        <value>turbo</value>
+                    </powertrain>
+                    <type description="Type of main thrust generator. Selector: fan / prop">
+                        <value>fan</value>
+                    </type>
+                    <position description="propulsor position (arrangement order acc to ID order)">
+                        <parent_component description="position on component. Selector: wing / fuselage / empennage">
+                            <value>wing</value>
+                        </parent_component>
+                        <x description="x-position (aircraft coordinate system). Selector: front / back">
+                            <value>front</value>
+                        </x>
+                        <y description="y position (aircraft coordinate system). Selector: left / right">
+                            <value>right</value>
+                        </y>
+                        <z description="z position (aircraft coordinate system). Selector: over / mid / under / in">
+                            <value>under</value>
+                        </z>
+                    </position>
+                    <energy_carrier_ID description="see energy carrier specification node">
+                        <value>777</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </energy_carrier_ID>
+                    <thrust_share description="Share of this thrust in relation to required aircraft thrust">
+                        <value>0.5</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </thrust_share>
+                </propulsor>
+                <energy_provider description="source where energy is coming from per segment">
+                    <ground description="source where energy is coming from in the ground mission segment">
+                        <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+                            <value>turbo</value>
+                        </powertrain>
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </ground>
+                    <taxi description="source where energy is coming from in the taxi mission segment">
+                        <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+                            <value>turbo</value>
+                        </powertrain>
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi>
+                    <takeoff description="source where energy is coming from in the takeoff mission segment">
+                        <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+                            <value>turbo</value>
+                        </powertrain>
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff>
+                    <climb description="source where energy is coming from in the climb mission segment">
+                        <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+                            <value>turbo</value>
+                        </powertrain>
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </climb>
+                    <cruise description="source where energy is coming from in the cruise mission segment">
+                        <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+                            <value>turbo</value>
+                        </powertrain>
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </cruise>
+                    <descent description="source where energy is coming from in the descent mission segment">
+                        <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+                            <value>turbo</value>
+                        </powertrain>
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </descent>
+                    <landing description="source where energy is coming from in the landing mission segment">
+                        <powertrain description="Way the power is generated from the source: propulsor, turbo, electric, fuel_cell">
+                            <value>turbo</value>
+                        </powertrain>
+                        <energy_carrier_ID description="see energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing>
+                </energy_provider>
+            </propulsion>
+            <skinning description="Skinning Information">
+                <material description="Material of skinning">
+                    <value>aluminium2024</value>
+                </material>
+                <thickness description="Thickness of skinning">
+                    <value>0.003</value>
+                    <unit>m</unit>
+                    <lower_boundary>0.0001</lower_boundary>
+                    <upper_boundary>0.1</upper_boundary>
+                </thickness>
+            </skinning>
+            <technology>
+                <variable_camber description="Switch if variable camber is used">
+                    <value>false</value>
+                </variable_camber>
+            </technology>
+        </design_specification>
+        <requirements description="Aircraft design requirements">
+            <top_level_aircraft_requirements description="Top level aircraft requirements (TLAR)">
+                <maximum_structrual_payload_mass description="Maximum structual payload mass which can be carried by the aircraft (e.g. for short trips)">
+                    <value>19300</value>
+                    <unit>kg</unit>
+                    <lower_boundary>100</lower_boundary>
+                    <upper_boundary>150000</upper_boundary>
+                </maximum_structrual_payload_mass>
+                <takeoff_distance description="Design takeoff distance (Balanced Field Length) at Sea Level with maximum takeoff mass (MTOM) and (ISA + deltaISA)-Conditions">
+                    <value>1951</value>
+                    <unit>m</unit>
+                    <lower_boundary>600</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </takeoff_distance>
+                <landing_field_length description="Needed runway length at Sea Level with maximum landiung mass (MLM) and (ISA + deltaISA)-Conditions (Safety-Landing Distance according to FAR 121.195: landing_field_required/0.6)">
+                    <value>2425.67</value>
+                    <unit>m</unit>
+                    <lower_boundary>600</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </landing_field_length>
+                <icao_aerodrome_reference_code description="ICAO reference code - code_number 1-4 (field length) + code_letter A-F (wing span limits) + faa ADG code number I-VI (wing span limits + tail height limits) + Aircraft Approach Category letter  A-D">
+                    <value>3CIIIB</value>
+                </icao_aerodrome_reference_code>
+                <flight_envelope description="Maxima of design flight envelope">
+                    <maximum_operating_mach_number description="Maximum operating mach number">
+                        <value>0.82</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_operating_mach_number>
+                    <maximum_operating_velocity description="Maximum operating speed (maximum dynamic pressure)">
+                        <value>180</value>
+                        <unit>m/s</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>250</upper_boundary>
+                    </maximum_operating_velocity>
+                    <maximum_approach_speed description="Maximum allowed approach speed.">
+                        <value>67.65</value>
+                        <unit>m/s</unit>
+                        <lower_boundary>50</lower_boundary>
+                        <upper_boundary>90</upper_boundary>
+                    </maximum_approach_speed>
+                    <maximum_operating_altitude description="Maximum operating altitude">
+                        <value>12192</value>
+                        <unit>m</unit>
+                        <lower_boundary>4500</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </maximum_operating_altitude>
+                    <maximum_altitude_one_engine_inoperative description="Maximum operating altitude with one engine inoperative">
+                        <value>4572</value>
+                        <unit>m</unit>
+                        <lower_boundary>1500</lower_boundary>
+                        <upper_boundary>12000</upper_boundary>
+                    </maximum_altitude_one_engine_inoperative>
+                    <climb_or_descend_segment_gradient description="climb / descend segment gradient">
+                        <value>0.024</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </climb_or_descend_segment_gradient>
+                </flight_envelope>
+                <pavement_classification_number description="Runway pavment classification number (PCN) - limits the maximum allowed aircraft classification number of undercarriage.">
+                    <value>55</value>
+                    <unit>1</unit>
+                    <lower_boundary>5</lower_boundary>
+                    <upper_boundary>120</upper_boundary>
+                </pavement_classification_number>
+                <design_mission description="Requirements regarding the design mission">
+                    <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+                        <value>0</value>
+                        <unit>K</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </delta_ISA>
+                    <range description="Target range for the specified mission">
+                        <value>4537400</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>20000000</upper_boundary>
+                    </range>
+                    <contingency description="Reserved Fuel Percentage">
+                        <value>0.06</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>0.08</upper_boundary>
+                    </contingency>
+                    <alt_dist description="Reserved fuel - alternate distance">
+                        <value>370400</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>926000</upper_boundary>
+                    </alt_dist>
+                    <loiter_time description="Reserved fuel - loiter time in seconds">
+                        <value>1800</value>
+                        <unit>s</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>3600</upper_boundary>
+                    </loiter_time>
+                    <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise.">
+                        <value>0.78</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </initial_cruise_mach_number>
+                    <initial_cruise_altitude description="Initial cruise altitude (ICA) at top of descent. May be altered during cruise.">
+                        <value>10058.4</value>
+                        <unit>m</unit>
+                        <lower_boundary>1000</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </initial_cruise_altitude>
+                    <climb_speed_schedule description="Climb speed for different altitudes">
+                        <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_below_FL100>
+                        <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_above_FL100>
+                        <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+                            <value>-0.02</value>
+                            <unit>1</unit>
+                            <lower_boundary>-0.3</lower_boundary>
+                            <upper_boundary>0.01</upper_boundary>
+                        </delta_mach_climb_cruise>
+                    </climb_speed_schedule>
+                    <descent_speed_schedule description="Descent speed for different altitudes">
+                        <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_below_FL100>
+                        <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_above_FL100>
+                    </descent_speed_schedule>
+                    <time_to_climb description="Time the aircraft takes to climb to cruise altitude">
+                        <value>2100</value>
+                        <unit>s</unit>
+                        <lower_boundary>600</lower_boundary>
+                        <upper_boundary>3600</upper_boundary>
+                    </time_to_climb>
+                    <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+                        <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
+                            <value>mode_0</value>
+                        </fuel_estimation_selector>
+                    </fuel_planning>
+                </design_mission>
+                <study_mission description="Requirements regarding the study mission">
+                    <delta_ISA description="Temperature offset to the International Standard Atmosphere (ISA)">
+                        <value>0</value>
+                        <unit>K</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </delta_ISA>
+                    <range description="Target range for the specified mission">
+                        <value>1481600</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>20000000</upper_boundary>
+                    </range>
+                    <initial_cruise_mach_number description="Initial cruise Mach number at top of descent. May be altered during cruise.">
+                        <value>0.78</value>
+                        <unit>1</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </initial_cruise_mach_number>
+                    <initial_cruise_altitude description="Initial cruise altitude at top of descent. May be altered during cruise.">
+                        <value>10668</value>
+                        <unit>m</unit>
+                        <lower_boundary>1000</lower_boundary>
+                        <upper_boundary>20000</upper_boundary>
+                    </initial_cruise_altitude>
+                    <climb_speed_schedule description="Climb speed for different altitudes">
+                        <climb_speed_below_FL100 description="Calibrated airspeed in climb below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_below_FL100>
+                        <climb_speed_above_FL100 description="Calibrated airspeed in climb above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </climb_speed_above_FL100>
+                        <delta_mach_climb_cruise description="Difference between crossover altitude Mach number and cruise Mach number">
+                            <value>-0.02</value>
+                            <unit>1</unit>
+                            <lower_boundary>-0.3</lower_boundary>
+                            <upper_boundary>0.01</upper_boundary>
+                        </delta_mach_climb_cruise>
+                    </climb_speed_schedule>
+                    <descent_speed_schedule description="Descent speed for different altitudes">
+                        <descent_speed_below_FL100 description="Calibrated airspeed in descent below FL100 (FL100 = 3048 m)">
+                            <value>128.6112</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_below_FL100>
+                        <descent_speed_above_FL100 description="Calibrated airspeed in descent above FL100 (FL100 = 3048 m)">
+                            <value>154.3334</value>
+                            <unit>m/s</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>250</upper_boundary>
+                        </descent_speed_above_FL100>
+                    </descent_speed_schedule>
+                    <fuel_planning description="Fuel planning according to the Joint Aviation Requirements (JAR) or the Federal Aviation Regulations (FAR)">
+                        <fuel_estimation_selector description="Fuel estimation method. Selector: mode_0 (Fuel planning according to JAR) / mode_1 (Domestic fuel planning according to FAR) / mode_2 (Flag or supplemental fuel planning according to FAR)">
+                            <value>mode_0</value>
+                        </fuel_estimation_selector>
+                    </fuel_planning>
+                    <payload_fractions description="Set the fraction of different design payload values for the study mission">
+                        <cargo_fraction description="Fraction of the design cargo mass which is used for the study mission">
+                            <value>0.75</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </cargo_fraction>
+                        <passenger_mass_fraction description="Fraction of the design passenger mass which is used for the study mission">
+                            <value>0.75</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </passenger_mass_fraction>
+                    </payload_fractions>
+                </study_mission>
+            </top_level_aircraft_requirements>
+            <additional_requirements description="Additional requirements">
+                <landing_gear description="Landing gear requirements and operational conditions">
+                    <friction_coefficient description="Friction coefficient of tyres and pavement: Raymer p.486 - Table 17.1: 0.03 - 0.05">
+                        <value>0.03</value>
+                        <default>0.03</default>
+                        <unit>1</unit>
+                        <lower_boundary>0.02</lower_boundary>
+                        <upper_boundary>0.08</upper_boundary>
+                    </friction_coefficient>
+                    <breaking_coefficient description="Raymer p.486 - Table 17.1: 0.3 - 0.5; Torenbeek: jet 0.4-0.5; prop 0.35-0.45; Airbus: Medium Deceleration = 11 ft/s^2 = 0.34189">
+                        <value>0.34189</value>
+                        <default>0.34189</default>
+                        <unit>1</unit>
+                        <lower_boundary>0.06</lower_boundary>
+                        <upper_boundary>0.5</upper_boundary>
+                    </breaking_coefficient>
+                </landing_gear>
+            </additional_requirements>
+        </requirements>
+        <assessment_scenario description="Scenario for ecological and economical assessment">
+            <flights_per_year description="Number of flights per year">
+                <value>2227</value>
+                <unit>1</unit>
+                <lower_boundary>0</lower_boundary>
+                <upper_boundary>4000</upper_boundary>
+            </flights_per_year>
+            <duration_operation description="Operating years of aircraft">
+                <value>25</value>
+                <unit>a</unit>
+                <lower_boundary>0</lower_boundary>
+                <upper_boundary>50</upper_boundary>
+            </duration_operation>
+        </assessment_scenario>
+    </requirements_and_specifications>
+    <analysis>
+        <masses_cg_inertia description="Masses, Center of Gravity, Inertias." tool_level="2">
+            <maximum_takeoff_mass description="MTOM">
+                <mass_properties description="maximum takeoff mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1510141.8121567257</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3738773.1116968105</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>5290910.387611725</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.378433652526235</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.4654642512511066</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>0</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_takeoff_mass>
+            <operating_mass_empty description="OME">
+                <mass_properties description="operating mass empty properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>820612.3650779686</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>2031652.5381796542</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2875085.274536487</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.108078043920829</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.7480947757156718</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>0</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </operating_mass_empty>
+            <manufacturer_mass_empty description="MME">
+                <mass_properties description="manufacturer mass empty properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>755918.7865518769</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>1871485.7181196488</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2648425.8152194647</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.04983525477432</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.8121168624538313</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>39545.4300408</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </manufacturer_mass_empty>
+            <maximum_zero_fuel_mass description="MZFM">
+                <mass_properties description="maximum zero fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1189535.7164083032</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>2945024.179920398</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4167639.640009298</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.6372561241248</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.5909171268946131</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>62229.835124</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_zero_fuel_mass>
+            <maximum_payload_mass description="">
+                <mass_properties description="maximum payload mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>16.8143301</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.2413</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>19300.0</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_payload_mass>
+            <maximum_landing_mass description="MLM">
+                <mass_properties description="maximum landing mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1273324.0627619973</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3152465.3711376246</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>4461199.243825872</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.108078043920829</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.7480947757156718</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>66613.1713340691</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_landing_mass>
+            <maximum_fuel_mass description="">
+                <mass_properties description="maximum fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>16.397420927086102</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.1257429972004459</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>22856.426473317864</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </maximum_fuel_mass>
+            <ferry_range_mass description="">
+                <mass_properties description="ferry range mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.556040431392383</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.5318682062042068</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>65786.26159731786</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </ferry_range_mass>
+            <most_forward_mass description="">
+                <mass_properties description="most forward mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>820612.3650779686</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>2031652.5381796542</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2875085.274536487</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.505998794238808</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>65462.14738244548</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </most_forward_mass>
+            <most_afterward_mass description="">
+                <mass_properties description="most afterward mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>820612.3650779686</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>2031652.5381796542</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>2875085.274536487</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.764874650500401</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>67862.14738244549</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </most_afterward_mass>
+            <design_mass description="">
+                <mass_properties description="design mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>1510141.8121567257</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>3738773.1116968105</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>5290910.387611725</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>15.378433652526235</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>-0.4654642512511066</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>79002.14738244547</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </design_mass>
+            <design_fuel_mass description="">
+                <mass_properties description="design fuel mass properties">
+                    <inertia description="Inertia with regard to the total center of gravity.">
+                        <j_xx description="Inertia in x.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xx>
+                        <j_yy description="Inertia in y.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yy>
+                        <j_zz description="Inertia in z.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zz>
+                        <j_xy description="Inertia in xy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xy>
+                        <j_xz description="Inertia in xz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_xz>
+                        <j_yx description="Inertia in yx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yx>
+                        <j_yz description="Inertia in yz.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_yz>
+                        <j_zx description="Inertia in zx.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zx>
+                        <j_zy description="Inertia in zy.">
+                            <value>0.0</value>
+                            <unit>kgm^2</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </j_zy>
+                    </inertia>
+                    <center_of_gravity description="Center of gravity w.r.t global coordinate system.">
+                        <x description="Center of gravity in x-direction with regard to the global reference point.">
+                            <value>14.412288484467158</value>
+                            <unit>m</unit>
+                            <lower_boundary>-100</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </x>
+                        <y description="Center of gravity in y-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-50</lower_boundary>
+                            <upper_boundary>50</upper_boundary>
+                        </y>
+                        <z description="Center of gravity in z-direction with regard to the global reference point.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-10</lower_boundary>
+                            <upper_boundary>10</upper_boundary>
+                        </z>
+                    </center_of_gravity>
+                    <mass description="Mass">
+                        <value>16992.947341067287</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </mass>
+                </mass_properties>
+            </design_fuel_mass>
+        </masses_cg_inertia>
+        <aerodynamics description="Aerodynamical analysis" tool_level="3">
+            <polar>
+                <polar_file description="Name of polar file">
+                    <value>SMR-2020_design_trimmed_polar.xml</value>
+                </polar_file>
+                <configurations description="Number of configurations in the polar file">
+                    <value>7</value>
+                    <unit>1</unit>
+                    <lower_boundary>-2147483648</lower_boundary>
+                    <upper_boundary>2147483647</upper_boundary>
+                </configurations>
+                <configuration ID="0" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>cruise</value>
+                    </type>
+                    <name description=" Name">
+                        <value>clean</value>
+                    </name>
+                </configuration>
+                <configuration ID="1" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>takeoff</value>
+                    </name>
+                </configuration>
+                <configuration ID="2" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>takeoff_landing_gear_retracted</value>
+                    </name>
+                </configuration>
+                <configuration ID="3" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>departure</value>
+                    </type>
+                    <name description=" Name">
+                        <value>climb</value>
+                    </name>
+                </configuration>
+                <configuration ID="4" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>approach</value>
+                    </name>
+                </configuration>
+                <configuration ID="5" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>approach_landing_gear_out</value>
+                    </name>
+                </configuration>
+                <configuration ID="6" description="Configuration in polar file marked with ID - name can vary">
+                    <type description=" Type">
+                        <value>approach</value>
+                    </type>
+                    <name description=" Name">
+                        <value>landing</value>
+                    </name>
+                </configuration>
+            </polar>
+            <reference_values>
+                <b description="Wing half span">
+                    <value>35.45215648</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </b>
+                <MAC description="Mean aerodynamic chord">
+                    <value>4.159695001</value>
+                    <unit>m</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </MAC>
+                <S_ref description="Wing reference area">
+                    <value>122.024796</value>
+                    <unit>m^2</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </S_ref>
+                <neutral_point>
+                    <x description="x component of neutral point">
+                        <value>16.54053159</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                </neutral_point>
+            </reference_values>
+            <lift_coefficients>
+                <C_LoptimumCruise description="C_LoptimumCruise">
+                    <value>0.549</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LoptimumCruise>
+                <C_LmaxLanding description="C_LmaxLanding">
+                    <value>2.135</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LmaxLanding>
+                <C_LmaxT-O description="C_LmaxTO">
+                    <value>1.981</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LmaxT-O>
+                <C_LgroundRoll description="C_LgroundRoll">
+                    <value>0.4</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </C_LgroundRoll>
+            </lift_coefficients>
+            <max_spoiler_factor description="max_spoiler_factor">
+                <value>2.5</value>
+                <unit>1</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </max_spoiler_factor>
+        </aerodynamics>
+        <mission description="Mission data" tool_level="0">
+            <design_mission description="Data of design mission">
+                <range description="Traveled range from break release to end of taxi at destination">
+                    <value>4538397.521</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>5000000</upper_boundary>
+                </range>
+                <loaded_mission_energy description="Amount of energy loaded into tanks (including reserves) for the mission">
+                    <mission_energy ID="0" description="Amount of energy loaded into tanks (including reserves) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7.323960304e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+12</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </mission_energy>
+                </loaded_mission_energy>
+                <in_flight_energy description="Amount of energy needed for in-flight segments (all segments from takeoff to landing)">
+                    <trip_energy ID="0" description="Amount of energy needed for trip segments (all segments from takeoff to landing) for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>6.022727396e+11</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+12</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </trip_energy>
+                    <takeoff_energy ID="0" description="Amount of energy needed for takeoff segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>8371897678</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+12</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </takeoff_energy>
+                    <landing_energy ID="0" description="Amount of energy needed for landing segment for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>7153542456</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+12</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </landing_energy>
+                </in_flight_energy>
+                <taxi_energy description="Amount of energy needed for taxiing specified energy carrier">
+                    <taxi_out_energy ID="0" description="Amount of energy needed for taxiing at origin for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>9509372061</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+12</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_out_energy>
+                    <taxi_in_energy ID="0" description="Amount of energy needed for taxiing at destination for specified energy carrier">
+                        <consumed_energy description="Energy amount">
+                            <value>5282984478</value>
+                            <unit>J</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1e+12</upper_boundary>
+                        </consumed_energy>
+                        <energy_carrier_ID description="See energy carrier specification node">
+                            <value>0</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </energy_carrier_ID>
+                    </taxi_in_energy>
+                </taxi_energy>
+                <block_time description="Block time for the whole mission: Time from break release to end of taxiing after landing">
+                    <value>21018.43583</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>45000</upper_boundary>
+                </block_time>
+                <flight_time description="Flight time for the whole mission">
+                    <value>20178.43583</value>
+                    <unit>s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>44500</upper_boundary>
+                </flight_time>
+                <takeoff_engine_derate description="Engine power demand">
+                    <value>1</value>
+                    <unit>1</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1</upper_boundary>
+                </takeoff_engine_derate>
+                <cruise description="Characteristics of the cruise segment">
+                    <average_lift_coefficient description="Lift coefficient CL_average: Arithmetic mean over the entire cruise flight">
+                        <value>0.5359768657</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </average_lift_coefficient>
+                    <minimum_lift_coefficient description="Minimum cruise flight lift coefficient CL_min">
+                        <value>0.5119970814</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </minimum_lift_coefficient>
+                    <maximum_lift_coefficient description="Maximum cruise flight lift coefficient CL_max">
+                        <value>0.5853999993</value>
+                        <unit>1</unit>
+                        <lower_boundary>-0.01</lower_boundary>
+                        <upper_boundary>1</upper_boundary>
+                    </maximum_lift_coefficient>
+                    <top_of_climb_mass description="Total aircraft mass at top of climb (= start of initial cruise altitude (ICA))">
+                        <value>77169.13482</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_climb_mass>
+                    <top_of_descent_mass description="Total aircraft mass at top of descent (TOD)">
+                        <value>65413.90831</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>150000</upper_boundary>
+                    </top_of_descent_mass>
+                    <top_of_climb_range description="Flown range from takeoff to top of climb (= start of initial cruise altitude (ICA))">
+                        <value>322125.6425</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>500000</upper_boundary>
+                    </top_of_climb_range>
+                    <top_of_descent_range description="Flown range from takeoff to top of descent">
+                        <value>4342074.947</value>
+                        <unit>kg</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>5000000</upper_boundary>
+                    </top_of_descent_range>
+                    <cruise_steps description="Cruise step information">
+                        <cruise_step ID="0" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>0.4991304067</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10058.4002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                        <cruise_step ID="1" description="Data of a cruise step">
+                            <relative_end_of_cruise_step description="End of cruise step relative to total cruise length">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </relative_end_of_cruise_step>
+                            <altitude description="Altitude of cruise step">
+                                <value>10668.0002</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>15000</upper_boundary>
+                            </altitude>
+                        </cruise_step>
+                    </cruise_steps>
+                </cruise>
+            </design_mission>
+        </mission>
+    </analysis>
+    <component_design>
+        <global_reference_point>
+            <reference_component description="Global reference point of aircraft geometry">
+                <value>fuselage</value>
+            </reference_component>
+            <x description="X coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </x>
+            <y description="Y coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </y>
+            <z description="Z coordinate of the global reference point">
+                <value>0</value>
+                <unit>m</unit>
+                <lower_boundary>-inf</lower_boundary>
+                <upper_boundary>inf</upper_boundary>
+            </z>
+        </global_reference_point>
+        <wing>
+            <mass_properties description="mass_properties of component wing">
+                <mass description="component mass">
+                    <value>8860.090873</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="wing inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="wing inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="wing inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="wing inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="wing inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="wing inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="wing inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="wing inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="wing inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>15.72374237</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>-0.6303854434</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <position description="position of wing">
+                <x description="x position">
+                    <value>11.51890797</value>
+                    <unit>1</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </x>
+                <y description="y position">
+                    <value>0</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z position">
+                    <value>-1.030445071</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <specific>
+                <geometry>
+                    <aerodynamic_surface ID="0" description="main_wing">
+                        <name description="name of surface">
+                            <value>main_wing</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>true</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>6.122921737</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1.00040016</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-1.983993414</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>6.122921737</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1.00040016</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="2">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>2.206655466</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0.2916723362</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-5.317823472</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>4.090984901</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>0.9140197858</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                                <section ID="3">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>9.291499097</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>1.377253963</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-17.72607824</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>1.040896695</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>0.5925187878</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>F15_15</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="slat">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1141636212</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.294</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.6981317008</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="1" description="slat">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.306</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.95</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.6981317008</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="2" description="flap_fowler">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1141636212</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.297</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="3" description="flap_fowler">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.303</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.75</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.78</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="4" description="aileron">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.8</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.98</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.3490658504</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.3490658504</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="5" description="spoiler_ground">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.2040818106</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.294</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="6" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.306</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.4195</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="7" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.4195</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.533</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="8" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.533</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.6465</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                                <control_device ID="9" description="spoiler_air">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.6465</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.85</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.76</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>0</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.7853981634</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                    </aerodynamic_surface>
+                </geometry>
+            </specific>
+        </wing>
+        <empennage>
+            <position description="position of empennage">
+                <x description="x position">
+                    <value>30.84621438</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </x>
+                <y description="y position">
+                    <value>0</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z position">
+                    <value>0.92429206</value>
+                    <unit>1</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="mass_properties of component Conventional tail overall mass">
+                <mass description="component mass">
+                    <value>1284.974715</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="Conventional tail overall mass inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Conventional tail overall mass inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Conventional tail overall mass inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Conventional tail overall mass inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Conventional tail overall mass inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Conventional tail overall mass inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Conventional tail overall mass inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Conventional tail overall mass inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Conventional tail overall mass inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>34.87847331</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>3.018558414</value>
+                        <unit>m</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific>
+                <geometry>
+                    <aerodynamic_surface ID="0" description="vertical_stabiliser">
+                        <name description="name of surface">
+                            <value>vertical_stabiliser</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>false</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>4.944968251</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>5.218300973</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-6.444065044</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>1.31140558</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="rudder">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.9</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                    </aerodynamic_surface>
+                    <aerodynamic_surface ID="1" description="horizontal_stabiliser">
+                        <name description="name of surface">
+                            <value>horizontal_stabiliser</value>
+                        </name>
+                        <position description="reference position in aircraft coordinates">
+                            <x description="x coordinate of point">
+                                <value>2.214733313</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-0.5869147662</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <parameters description="aerodynamic surface parameters">
+                            <direction description="unit vector according to aircraft coordinate system for direction applied at position">
+                                <x description="x direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y direction of unit vector">
+                                    <value>-1</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z direction of unit vector">
+                                    <value>0</value>
+                                    <unit>1</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </direction>
+                            <symmetric description="symmetric to local x-z plane">
+                                <value>true</value>
+                            </symmetric>
+                            <sections description="sections">
+                                <section ID="0">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>3.230234937</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                                <section ID="1">
+                                    <chord_origin description="origin of chord (local)">
+                                        <x description="x coordinate of point">
+                                            <value>3.532093643</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </x>
+                                        <y description="y coordinate of point">
+                                            <value>0.4945324201</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </y>
+                                        <z description="z coordinate of point">
+                                            <value>-5.652531425</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </z>
+                                    </chord_origin>
+                                    <chord_length description="chord length of the section">
+                                        <value>0.911572299</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </chord_length>
+                                    <geometric_twist description="geometric twist of the section around leading edge">
+                                        <value>-0</value>
+                                        <unit>rad</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </geometric_twist>
+                                    <scale_thickness description="scale the thickness defined by the profile with this factor">
+                                        <value>1</value>
+                                        <unit>1</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </scale_thickness>
+                                    <profile description="profile (data normalized to chord length)">
+                                        <value>n0012</value>
+                                    </profile>
+                                </section>
+                            </sections>
+                            <spars>
+                                <spar ID="0" description="front_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.2</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                                <spar ID="1" description="rear_spar">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>0.6</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-1</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                </spar>
+                            </spars>
+                            <control_devices>
+                                <control_device ID="0" description="elevator">
+                                    <position description="relative chord position">
+                                        <inner_position description="relative inner position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.2</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </inner_position>
+                                        <outer_position description="relative outer position">
+                                            <chord description="chord position">
+                                                <from description="relative chord position">
+                                                    <value>0.7</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </from>
+                                                <to description="relative chord position">
+                                                    <value>1</value>
+                                                    <unit>1</unit>
+                                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                                </to>
+                                            </chord>
+                                            <spanwise description="relative spanwise position">
+                                                <value>-0.9</value>
+                                                <unit>1</unit>
+                                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                                <upper_boundary>1.797693135e+308</upper_boundary>
+                                            </spanwise>
+                                        </outer_position>
+                                    </position>
+                                    <deflection>
+                                        <full_negative_deflection description="full negative deflection">
+                                            <value>-0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_negative_deflection>
+                                        <full_positive_deflection description="full positive deflection">
+                                            <value>0.4363323125</value>
+                                            <unit>rad</unit>
+                                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                                            <upper_boundary>1.797693135e+308</upper_boundary>
+                                        </full_positive_deflection>
+                                    </deflection>
+                                </control_device>
+                            </control_devices>
+                        </parameters>
+                    </aerodynamic_surface>
+                </geometry>
+            </specific>
+        </empennage>
+        <propulsion>
+            <position description="Reference position of the propulsion assembly">
+                <x description="x coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </x>
+                <y description="y coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </y>
+                <z description="z coordinate of point">
+                    <value>0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of the propulsion assembly">
+                <mass description="mass of the of the component">
+                    <value>9227.545786</value>
+                    <unit>kg</unit>
+                    <lower_boundary>-inf</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of the component in respect to the CG">
+                    <j_xx description="inertia of the component">
+                        <value>358507.5774</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="inertia of the component">
+                        <value>12053.92335</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="inertia of the component">
+                        <value>362014.3132</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="inertia of the component">
+                        <value>-0.04007228226</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="inertia of the component">
+                        <value>2014.79068</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="inertia of the component">
+                        <value>-0.04007228226</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="inertia of the component">
+                        <value>-0.003671168329</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="inertia of the component">
+                        <value>2014.79068</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="inertia of the component">
+                        <value>-0.003671168329</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                    <x description="x coordinate of the center of gravity">
+                        <value>13.39098398</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                    <y description="y coordinate of the center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </y>
+                    <z description="z coordinate of the center of gravity">
+                        <value>-2.45044457</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific>
+                <propulsion ID="0" description="Description of one propulsion">
+                    <nacelle ID="0" description="Nacelle of the propulsion assembly">
+                        <position description="Origin of the nacelle RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+                            <x description="x direction of unit vector">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="Geometrical description nacelle sections">
+                            <section ID="0">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0.858606747</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="2">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>2.575820241</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="3">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>3.434426988</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the nacelle">
+                            <mass description="mass of the of the component">
+                                <value>1044.421165</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>52.54222833</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>53.71263772</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>53.71822863</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.004167372537</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.004259196874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.004167372537</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0.0005734046682</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.004259196874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0.0005734046682</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>13.23123029</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.178624397</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.633399725</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </nacelle>
+                    <pylon ID="0" description="pylon of the propulsion assembly">
+                        <position description="Position of the pylon RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="unit vector according to aircraft coordinate system for direction applied at position">
+                            <x description="x direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>-1.125678464</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="sections">
+                            <section ID="0">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>1.378558528e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.125678464</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.434426988</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>2.703045251</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>2.412477425e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.969937313</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.434426988</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the pylon">
+                            <mass description="mass of the of the component">
+                                <value>545.3606608</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>0.6045290934</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>12.37643343</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>12.03331888</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.01586876859</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>1.402798952</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.01586876859</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.00240898882</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>1.402798952</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.00240898882</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>14.58275291</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.178624397</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-1.085591836</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </pylon>
+                    <engine>
+                        <model description="Name of selected engine model">
+                            <value>PW1127G-JM</value>
+                        </model>
+                        <position description="Position of the engine in the global coordinate system">
+                            <x description="x coordinate of point">
+                                <value>11.51401679</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>-6.178624397</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-2.633399725</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of the engine">
+                            <mass description="mass of the of the component">
+                                <value>3023.991067</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>1915.928172</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>3930.368067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>3930.368067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>13.23123029</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>-6.178624397</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.633399725</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <SLST description="Sea level static thrust of the engine">
+                            <value>123410.9874</value>
+                            <unit>N</unit>
+                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </SLST>
+                        <scale_factor description="Scale factor of the engine">
+                            <value>1.024752864</value>
+                            <unit>1</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </scale_factor>
+                        <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+                            <thrust description="Thrust of the engine at the bucket point">
+                                <value>20359.19396</value>
+                                <unit>N</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </thrust>
+                            <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+                                <value>1.505601144e-05</value>
+                                <unit>kg/Ns</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </tsfc>
+                        </bucket_point>
+                    </engine>
+                </propulsion>
+                <propulsion ID="1" description="Description of one propulsion">
+                    <nacelle ID="0" description="Nacelle of the propulsion assembly">
+                        <position description="Origin of the nacelle RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="Normal direction of the nacelle in the global aircraft coordinate system">
+                            <x description="x direction of unit vector">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="Geometrical description nacelle sections">
+                            <section ID="0">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>0.858606747</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="2">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>2.575820241</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.814196161</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                            <section ID="3">
+                                <origin description="Origin of the section (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>3.434426988</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <width description="width of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </width>
+                                <height description="Height of the section">
+                                    <value>2.251356929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </height>
+                                <profile description="The profile name of the section">
+                                    <value>nacelle</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the nacelle">
+                            <mass description="mass of the of the component">
+                                <value>1044.421165</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>52.54222833</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>53.71263772</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>53.71822863</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.004167372537</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0.004259196874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.004167372537</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0.0005734046682</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0.004259196874</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0.0005734046682</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>13.23123029</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.178624397</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.633399725</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </nacelle>
+                    <pylon ID="0" description="pylon of the propulsion assembly">
+                        <position description="Position of the pylon RELATIVE to the engine position.">
+                            <x description="x coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <normal description="unit vector according to aircraft coordinate system for direction applied at position">
+                            <x description="x direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y direction of unit vector">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z direction of unit vector">
+                                <value>-1.125678464</value>
+                                <unit>1</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </normal>
+                        <sections description="sections">
+                            <section ID="0">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>1.378558528e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.125678464</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.434426988</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                            <section ID="1">
+                                <origin description="origin of chord (local)">
+                                    <x description="x coordinate of point">
+                                        <value>2.703045251</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </x>
+                                    <y description="y coordinate of point">
+                                        <value>2.412477425e-16</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </y>
+                                    <z description="z coordinate of point">
+                                        <value>-1.969937313</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                                        <upper_boundary>1.797693135e+308</upper_boundary>
+                                    </z>
+                                </origin>
+                                <chord_length description="chord length of the section">
+                                    <value>3.434426988</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </chord_length>
+                                <geometric_twist description="geometric twist of the section around leading edge">
+                                    <value>-0</value>
+                                    <unit>rad</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </geometric_twist>
+                                <profile description="profile (data normalized to chord length)">
+                                    <value>pylon</value>
+                                </profile>
+                            </section>
+                        </sections>
+                        <mass_properties description="Mass properties of the pylon">
+                            <mass description="mass of the of the component">
+                                <value>545.3606608</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>0.6045290934</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>12.37643343</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>12.03331888</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>-0.01586876859</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>1.402798952</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>-0.01586876859</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>-0.00240898882</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>1.402798952</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>-0.00240898882</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>14.58275291</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.178624397</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-1.085591836</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                    </pylon>
+                    <engine>
+                        <model description="Name of selected engine model">
+                            <value>PW1127G-JM</value>
+                        </model>
+                        <position description="Position of the engine in the global coordinate system">
+                            <x description="x coordinate of point">
+                                <value>11.51401679</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y coordinate of point">
+                                <value>6.178624397</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z coordinate of point">
+                                <value>-2.633399725</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of the engine">
+                            <mass description="mass of the of the component">
+                                <value>3023.991067</value>
+                                <unit>kg</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of the component in respect to the CG">
+                                <j_xx description="inertia of the component">
+                                    <value>1915.928172</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xx>
+                                <j_yy description="inertia of the component">
+                                    <value>3930.368067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yy>
+                                <j_zz description="inertia of the component">
+                                    <value>3930.368067</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zz>
+                                <j_xy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xy>
+                                <j_xz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_xz>
+                                <j_yx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yx>
+                                <j_yz description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_yz>
+                                <j_zx description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zx>
+                                <j_zy description="inertia of the component">
+                                    <value>0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-1.797693135e+308</lower_boundary>
+                                    <upper_boundary>1.797693135e+308</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of the component with respect to the global coordinate system">
+                                <x description="x coordinate of the center of gravity">
+                                    <value>13.23123029</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </x>
+                                <y description="y coordinate of the center of gravity">
+                                    <value>6.178624397</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </y>
+                                <z description="z coordinate of the center of gravity">
+                                    <value>-2.633399725</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <SLST description="Sea level static thrust of the engine">
+                            <value>123410.9874</value>
+                            <unit>N</unit>
+                            <lower_boundary>-1.797693135e+308</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </SLST>
+                        <scale_factor description="Scale factor of the engine">
+                            <value>1.024752864</value>
+                            <unit>1</unit>
+                            <lower_boundary>-inf</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </scale_factor>
+                        <bucket_point description="Bucket point of the engine at initial cruise flight phase">
+                            <thrust description="Thrust of the engine at the bucket point">
+                                <value>20359.19396</value>
+                                <unit>N</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </thrust>
+                            <tsfc description="Thrust specific fuel consumption of the engine at the bucket point">
+                                <value>1.505601144e-05</value>
+                                <unit>kg/Ns</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </tsfc>
+                        </bucket_point>
+                    </engine>
+                </propulsion>
+            </specific>
+        </propulsion>
+        <systems>
+            <mass_properties description="mass_properties of component systems">
+                <mass description="component mass">
+                    <value>5446.81491</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>1.797693135e+308</upper_boundary>
+                </mass>
+                <inertia description="component inertia referred to local center of gravity">
+                    <j_xx description="systems inertia in x">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xx>
+                    <j_yy description="systems inertia in y">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yy>
+                    <j_zz description="systems inertia in z">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zz>
+                    <j_xy description="systems inertia in xy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xy>
+                    <j_xz description="systems inertia in xz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_xz>
+                    <j_yx description="systems inertia in yx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yx>
+                    <j_yz description="systems inertia in yz">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_yz>
+                    <j_zx description="systems inertia in zx">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zx>
+                    <j_zy description="systems inertia in zy">
+                        <value>0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                    <x description="x position of center of gravity">
+                        <value>7.510092571</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </x>
+                    <y description="y position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </y>
+                    <z description="z position of center of gravity">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-1.797693135e+308</lower_boundary>
+                        <upper_boundary>1.797693135e+308</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <operator_items>
+                <operator_item ID="0">
+                    <name description="name of the operator item">
+                        <value>water_and_toilet_chemicals</value>
+                    </name>
+                    <mass_properties description="mass_properties of component water and toilet chemicals">
+                        <mass description="component mass">
+                            <value>244.8</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </mass>
+                        <inertia description="component inertia referred to local center of gravity">
+                            <j_xx description="water and toilet chemicals inertia in x">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xx>
+                            <j_yy description="water and toilet chemicals inertia in y">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yy>
+                            <j_zz description="water and toilet chemicals inertia in z">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zz>
+                            <j_xy description="water and toilet chemicals inertia in xy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xy>
+                            <j_xz description="water and toilet chemicals inertia in xz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xz>
+                            <j_yx description="water and toilet chemicals inertia in yx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yx>
+                            <j_yz description="water and toilet chemicals inertia in yz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yz>
+                            <j_zx description="water and toilet chemicals inertia in zx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zx>
+                            <j_zy description="water and toilet chemicals inertia in zy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                            <x description="x position of center of gravity">
+                                <value>3.061460869</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                    </mass_properties>
+                </operator_item>
+                <operator_item ID="1">
+                    <name description="name of the operator item">
+                        <value>residual_oil_and_fuel</value>
+                    </name>
+                    <mass_properties description="mass_properties of component water and toilet chemicals">
+                        <mass description="component mass">
+                            <value>0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1.797693135e+308</upper_boundary>
+                        </mass>
+                        <inertia description="component inertia referred to local center of gravity">
+                            <j_xx description="water and toilet chemicals inertia in x">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xx>
+                            <j_yy description="water and toilet chemicals inertia in y">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yy>
+                            <j_zz description="water and toilet chemicals inertia in z">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zz>
+                            <j_xy description="water and toilet chemicals inertia in xy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xy>
+                            <j_xz description="water and toilet chemicals inertia in xz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_xz>
+                            <j_yx description="water and toilet chemicals inertia in yx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yx>
+                            <j_yz description="water and toilet chemicals inertia in yz">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_yz>
+                            <j_zx description="water and toilet chemicals inertia in zx">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zx>
+                            <j_zy description="water and toilet chemicals inertia in zy">
+                                <value>0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="component center of gravity with respect to global coordinate system">
+                            <x description="x position of center of gravity">
+                                <value>15.72374237</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </x>
+                            <y description="y position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </y>
+                            <z description="z position of center of gravity">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-1.797693135e+308</lower_boundary>
+                                <upper_boundary>1.797693135e+308</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                    </mass_properties>
+                </operator_item>
+            </operator_items>
+            <specific>
+                <geometry>
+                    <mass_properties>
+                        <fuel_system description="mass of ATA-28">
+                            <value>260.2783506</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </fuel_system>
+                        <de_icing description="mass of ATA-30">
+                            <value>38.20847961</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </de_icing>
+                        <lighting description="mass of ATA-33">
+                            <value>232.9926862</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </lighting>
+                        <fire_protection description="mass of ATA-26">
+                            <value>84.37707073</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </fire_protection>
+                        <oxygen_system description="mass of ATA-35">
+                            <value>99.86208</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </oxygen_system>
+                        <flight_controls description="mass of ATA-27">
+                            <value>1207.855649</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </flight_controls>
+                        <instruments description="mass of ATA31">
+                            <value>76.35389846</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </instruments>
+                        <automatic_flight_system description="mass of ATA22">
+                            <value>124.075085</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </automatic_flight_system>
+                        <navigation description="mass of ATA34">
+                            <value>505.8445773</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </navigation>
+                        <communication description="mass of ATA23">
+                            <value>248.15017</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </communication>
+                        <bleed_air_system description="mass of ATA-36">
+                            <value>173.1963797</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </bleed_air_system>
+                        <hydraulic_generation description="mass of ATA-29">
+                            <value>118.1462372</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </hydraulic_generation>
+                        <hydraulic_distribution description="mass of ATA-29">
+                            <value>551.7045686</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </hydraulic_distribution>
+                        <electrical_generation description="mass of ATA-24">
+                            <value>522.4924205</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </electrical_generation>
+                        <electrical_distribution description="mass of ATA-24">
+                            <value>449.1695342</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </electrical_distribution>
+                        <auxiliary_power_unit description="mass of ATA-49">
+                            <value>173.7035449</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </auxiliary_power_unit>
+                        <air_conditioning description="mass of ATA-21">
+                            <value>335.6041788</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </air_conditioning>
+                    </mass_properties>
+                </geometry>
+                <maximium_power_demand description="maximum power (hydraulic + electric) demand">
+                    <value>232657.9673</value>
+                    <unit>W</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </maximium_power_demand>
+                <maximium_bleed_air_demand description="maximum bleed air demand">
+                    <value>2.157080241</value>
+                    <unit>kg/s</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </maximium_bleed_air_demand>
+                <average_power_demand description="average power (hydraulic + electric) demand">
+                    <value>60778.51494</value>
+                    <unit>W</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </average_power_demand>
+                <average_bleed_air_demand description="average bleed air demand">
+                    <value>1.024591634</value>
+                    <unit>W</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </average_bleed_air_demand>
+            </specific>
+        </systems>
+        <fuselage description="Geometric description of the aircraft fuselage." tool_level="1">
+            <position description="Position of the fuselages with regard to the global reference point.">
+                <x description="Distance in x direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-100</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </x>
+                <y description="Distance in y direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-25</lower_boundary>
+                    <upper_boundary>25</upper_boundary>
+                </y>
+                <z description="Distance in z direction with regard to the global reference point. (fuselage nose point)">
+                    <value>-0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-5</lower_boundary>
+                    <upper_boundary>5</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of all fuselages.">
+                <mass description="Mass of all fuselages.">
+                    <value>15542.96614</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of all fuselages with regard to the total center of gravity.">
+                    <j_xx description="Inertia of the of all fuselages in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of the of all fuselages in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of the of all fuselages in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of all fuselages in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of all fuselages in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of all fuselages in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of all fuselages in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of all fuselages in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of all fuselages in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of all fuselages.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point. (of all fuselages)">
+                        <value>16.8143301</value>
+                        <unit>m</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>50</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point. (of all fuselages)">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point. (of all fuselages)">
+                        <value>-0.2413</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific description="Fuselage design specific output parameter.">
+                <geometry description="Geometry description of the entire fuselage design.">
+                    <fuselage ID="0" description="Geometrical description of one entire fuselage.">
+                        <name description="Name of the fuselage.">
+                            <value>fuselage_0</value>
+                        </name>
+                        <position description="Position of one entire fuselage with regard to the fuselage global position.">
+                            <x description="Distance in x direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-25</lower_boundary>
+                                <upper_boundary>25</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the fuselage gear global position.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </position>
+                        <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                            <x description="X component of the unit vector.">
+                                <value>1</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </x>
+                            <y description="Y component of the unit vector.">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </y>
+                            <z description="Z component of the unit vector.">
+                                <value>0</value>
+                                <unit>1</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1</upper_boundary>
+                            </z>
+                        </direction>
+                        <mass_properties description="Mass properties of one entire fuselage.">
+                            <mass description="Mass of one entire fuselage.">
+                                <value>15542.966136707</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>100000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire fuselage with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire fuselage in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire fuselage in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire fuselage in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire fuselage in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire fuselage in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire fuselage in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire fuselage in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire fuselage in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire fuselage in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire fuselage.">
+                                <x description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-25</lower_boundary>
+                                    <upper_boundary>25</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global fuselage center of gravity position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <sections description="Geometrical description of the fuselage sections of one entire fuselage.">
+                            <section ID="0" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_0</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.957580772</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.068075648</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.236859405</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.267784187</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.496500597</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="1" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_1</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.924669034</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.192850112</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.410780143</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.467145347</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.836740921</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="2" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_2</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.88671607</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.325974005</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.51432337</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.617001451</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.09949371</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="3" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_3</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.814819481</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.552671561</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.638938798</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.811634047</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.332869486</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="4" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_4</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.746964181</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>0.779068819</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.756396515</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.976318453</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.597847703</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="5" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_5</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.624593025</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>1.123655542</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.945319536</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.21146329</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>1.950706682</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="6" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_6</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.499674101</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>1.438280013</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.097107435</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.429827854</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.243644807</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="7" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_7</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.21769763</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>2.128158942</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.34967515</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.867364888</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.796234326</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="8" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_8</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.174885536</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>2.619107088</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.558414858</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.971983901</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.095828445</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="9" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_9</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.083279283</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>3.445878719</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.734079899</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.113593806</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.508608277</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="10" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_10</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>-0.041639641</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>4.194982413</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.833938046</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.167125385</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.762303773</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="11" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_11</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>5.168818078</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.877197398</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.219197163</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.908262138</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="12" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_12</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>6.2175644</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915417119</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227075627</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="13" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_13</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>6.237748405</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915417119</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227075627</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="14" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_14</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>27.5216784</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915413925</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227071912</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="15" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_15</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>27.42759412</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.915413925</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>2.227071912</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.967986828</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="16" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_16</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>31.85324279</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.699062858</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.736603193</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.3288491</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="17" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_17</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>32.70160959</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.657090968</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>1.517243141</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>3.095828445</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="18" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_18</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>34.3983432</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>1.575335554</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.939595006</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>2.46334671</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                            <section ID="19" description="Geometrical description of one fuselage section.">
+                                <name description="Name of the fuselage section.">
+                                    <value>section_19</value>
+                                </name>
+                                <section_shape description="Contains a string with the path to the shape *.dat file or the key word: ellipse.">
+                                    <value>ellipse</value>
+                                </section_shape>
+                                <origin description="Origin of fuselage section (local).">
+                                    <x description="Distance in x direction with regard to the global reference point.">
+                                        <value>-0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the global reference point.">
+                                        <value>0.92429206</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the global reference point.">
+                                        <value>37.35925828</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-75</lower_boundary>
+                                        <upper_boundary>75</upper_boundary>
+                                    </z>
+                                </origin>
+                                <upper_height description="Height of the upper half of the fuselage section.">
+                                    <value>0.528165979</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </upper_height>
+                                <lower_height description="Height of the lower half of the fuselage section.">
+                                    <value>0.614104138</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </lower_height>
+                                <width description="Width of the fuselage section.">
+                                    <value>0.559150813</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </width>
+                            </section>
+                        </sections>
+                        <number_of_required_cabin_crew description="Number of minimum required flight attendants.">
+                            <value>4</value>
+                            <unit>1</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>100</upper_boundary>
+                        </number_of_required_cabin_crew>
+                        <mass_breakdown description="Mass breakdown of fuselage design module in accordance to CPACS.">
+                            <fuselage_structure description="Mass breakdown of the fuselage structure block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage structure block.">
+                                    <name description="Name of the fuselage structure component.">
+                                        <value>door_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage structure component.">
+                                        <value>360.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage structure block.">
+                                    <name description="Name of the fuselage structure component.">
+                                        <value>fuselage_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage structure component.">
+                                        <value>9049.071278727</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_structure>
+                            <fuselage_furnishing description="Mass breakdown of the fuselage furnishing block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>lavatory_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>290.01</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>flight_attendant_seat_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>48.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="2" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>floor_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>159.641751426</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="3" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>wall_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>289.30950138</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="4" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>ceiling_covering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>106.98516576</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="5" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>linings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>396.29466714</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="6" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>acoustic_and_thermal_insolation_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>619.536640625</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="7" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>overhead_bin_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>351.213928</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="8" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>passenger_safety_unit_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>90.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="9" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>lightning_panel_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>72.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="10" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>oxygen_system_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>201.51999999999998</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="11" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>cargo_linings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>319.955535336</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="12" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>cargo_loadings_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>264.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="13" description="Mass of a single component of the fuselage furnishing block.">
+                                    <name description="Name of the fuselage furnishing component.">
+                                        <value>miscellaneous_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage furnishing component.">
+                                        <value>272.217252253</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_furnishing>
+                            <fuselage_operator_items description="Mass breakdown of the fuselage  operator items block.">
+                                <component_mass ID="0" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_emergency_equipment_masses</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>260.48508319999996</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="1" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>flight_attendant_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>280.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="2" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>in_flight_entertainment</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>90.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="3" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_fixed_galley_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>315.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="4" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>total_seat_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>1242.0</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                                <component_mass ID="5" description="Mass of a single component of the fuselage  operator items block.">
+                                    <name description="Name of the fuselage operator items component.">
+                                        <value>catering_mass</value>
+                                    </name>
+                                    <mass description="Mass of the fuselage operator item component.">
+                                        <value>952.02</value>
+                                        <unit>kg</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>100000</upper_boundary>
+                                    </mass>
+                                </component_mass>
+                            </fuselage_operator_items>
+                        </mass_breakdown>
+                        <fuselage_accommodation description="Description of the accommodation of current fuselage.">
+                            <position description="Position of the payload tubes with regard to the fuselage position.">
+                                <x description="Distance in x direction with regard to the fuselage position.">
+                                    <value>3.75</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Distance in y direction with regard to the fuselage position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-0</lower_boundary>
+                                    <upper_boundary>0</upper_boundary>
+                                </y>
+                                <z description="Distance in z direction with regard to the fuselage position.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <mass_properties description="Mass properties of the payload tubes of one entire fuselage.">
+                                <mass description="Mass of the payload tubes of one entire fuselage.">
+                                    <value>6133.89485798</value>
+                                    <unit>kg</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>100000</upper_boundary>
+                                </mass>
+                                <center_of_gravity description="Center of gravity of all payload tubes.">
+                                    <x description="Center of gravity in x-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>0</lower_boundary>
+                                        <upper_boundary>50</upper_boundary>
+                                    </x>
+                                    <y description="Center of gravity in y-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-5</lower_boundary>
+                                        <upper_boundary>5</upper_boundary>
+                                    </y>
+                                    <z description="Center of gravity in z-direction with regard to the center of gravity of the fuselage.">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-5</lower_boundary>
+                                        <upper_boundary>5</upper_boundary>
+                                    </z>
+                                </center_of_gravity>
+                            </mass_properties>
+                            <payload_tube ID="0" description="Geometrical description of one payload tube of the fuselage.">
+                                <name description="Name of the payload tube.">
+                                    <value>center_payload_tube</value>
+                                </name>
+                                <payload_tube_reference_points description="Payload tube center reference points in x, y and z-direction referred to fuselage nose point.">
+                                    <front_reference_points description="Reference points in the front of payload tube.">
+                                        <x description="Payload tube reference point in x-direction.">
+                                            <value>0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <y description="Payload tube reference point in y-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </y>
+                                        <z description="Payload tube reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                        <upper_z description="Upper payload tube reference point in z-direction.">
+                                            <value>1.778</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </upper_z>
+                                        <lower_z description="Lower payload tube reference point in z-direction.">
+                                            <value>-2.089658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>0</upper_boundary>
+                                        </lower_z>
+                                    </front_reference_points>
+                                    <aft_reference_points description="Reference points in the aft of payload tube.">
+                                        <x description="Payload tube reference point in x-direction.">
+                                            <value>27.016456</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <y description="Payload tube reference point in y-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </y>
+                                        <z description="Payload tube reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                        <upper_z description="Upper payload tube reference point in z-direction.">
+                                            <value>1.778</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </upper_z>
+                                        <lower_z description="Lower payload tube reference point in z-direction.">
+                                            <value>-2.089658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>0</upper_boundary>
+                                        </lower_z>
+                                    </aft_reference_points>
+                                </payload_tube_reference_points>
+                                <payload_tube_wall_reference_points description="Payload tube wall reference points in x, y and z-direction referred to fuselage nose point.">
+                                    <front_reference_points description="Reference points in the front of payload tube.">
+                                        <x description="Wall reference point in x-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <left_y description="Left wall reference point in y-direction.">
+                                            <value>-1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </left_y>
+                                        <right_y description="Right wall reference point in y-direction.">
+                                            <value>1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </right_y>
+                                        <z description="Wall reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                    </front_reference_points>
+                                    <aft_reference_points description="Reference points in the aft of payload tube.">
+                                        <x description="Wall reference point in x-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-100</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </x>
+                                        <left_y description="Left wall reference point in y-direction.">
+                                            <value>-1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </left_y>
+                                        <right_y description="Right wall reference point in y-direction.">
+                                            <value>1.84658</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-35</lower_boundary>
+                                            <upper_boundary>35</upper_boundary>
+                                        </right_y>
+                                        <z description="Wall reference point in z-direction.">
+                                            <value>0.0</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>-15</lower_boundary>
+                                            <upper_boundary>15</upper_boundary>
+                                        </z>
+                                    </aft_reference_points>
+                                </payload_tube_wall_reference_points>
+                                <payload_tube_structural_wall_thickness description="Structural wall thickness of the payload tube.">
+                                    <value>0.137414</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </payload_tube_structural_wall_thickness>
+                                <payload_tube_water_volume description="Total water volume of one entire payload tube.">
+                                    <value>188.925079455</value>
+                                    <unit>m^3</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1000</upper_boundary>
+                                </payload_tube_water_volume>
+                                <payload_decks description="Geometrical description of the payload decks.">
+                                    <payload_deck ID="0" description="Geometrical description of the payload decks in one payload tube.">
+                                        <name description="Name of the payload deck.">
+                                            <value>passenger_deck_1</value>
+                                        </name>
+                                        <position description="Position of the payload deck with regard to the payload tube reference point.">
+                                            <x description="Distance in x direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-100</lower_boundary>
+                                                <upper_boundary>100</upper_boundary>
+                                            </x>
+                                            <y description="Distance in y direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-0</lower_boundary>
+                                                <upper_boundary>0</upper_boundary>
+                                            </y>
+                                            <z description="Distance in z direction with regard to the payload tube reference point.">
+                                                <value>-0.4826</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-5</lower_boundary>
+                                                <upper_boundary>5</upper_boundary>
+                                            </z>
+                                        </position>
+                                        <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+                                            <value>0.206248</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1</upper_boundary>
+                                        </payload_deck_structural_floor_thickness>
+                                        <payload_deck_water_volume description="Total water volume of the payload deck.">
+                                            <value>125.95005297</value>
+                                            <unit>m^3</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1000</upper_boundary>
+                                        </payload_deck_water_volume>
+                                        <payload_deck_length description="Total length of the payload deck.">
+                                            <value>27.016456</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </payload_deck_length>
+                                        <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+                                            <value>9000</value>
+                                            <unit>W</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100000</upper_boundary>
+                                        </payload_deck_required_galley_power>
+                                    </payload_deck>
+                                    <payload_deck ID="1" description="Geometrical description of the payload decks in one payload tube.">
+                                        <name description="Name of the payload deck.">
+                                            <value>cargo_deck</value>
+                                        </name>
+                                        <position description="Position of the payload deck with regard to the payload tube reference point.">
+                                            <x description="Distance in x direction with regard to the payload tube reference point.">
+                                                <value>3.75</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-100</lower_boundary>
+                                                <upper_boundary>100</upper_boundary>
+                                            </x>
+                                            <y description="Distance in y direction with regard to the payload tube reference point.">
+                                                <value>0.0</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-0</lower_boundary>
+                                                <upper_boundary>0</upper_boundary>
+                                            </y>
+                                            <z description="Distance in z direction with regard to the payload tube reference point.">
+                                                <value>-1.831848</value>
+                                                <unit>m</unit>
+                                                <lower_boundary>-5</lower_boundary>
+                                                <upper_boundary>5</upper_boundary>
+                                            </z>
+                                        </position>
+                                        <payload_deck_structural_floor_thickness description="Structural floor thickness of current payload deck.">
+                                            <value>0.206248</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1</upper_boundary>
+                                        </payload_deck_structural_floor_thickness>
+                                        <payload_deck_water_volume description="Total water volume of the payload deck.">
+                                            <value>62.975026485</value>
+                                            <unit>m^3</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>1000</upper_boundary>
+                                        </payload_deck_water_volume>
+                                        <payload_deck_length description="Total length of the payload deck.">
+                                            <value>13.508228</value>
+                                            <unit>m</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100</upper_boundary>
+                                        </payload_deck_length>
+                                        <payload_deck_required_galley_power description="Required galley power of the payload deck.">
+                                            <value>0</value>
+                                            <unit>W</unit>
+                                            <lower_boundary>0</lower_boundary>
+                                            <upper_boundary>100000</upper_boundary>
+                                        </payload_deck_required_galley_power>
+                                    </payload_deck>
+                                </payload_decks>
+                            </payload_tube>
+                        </fuselage_accommodation>
+                    </fuselage>
+                </geometry>
+            </specific>
+        </fuselage>
+        <tank description="Description of aircraft tanks." tool_level="2">
+            <position description="Tank reference point, position of the tanks with regard to the global reference point.">
+                <x description="Distance between the foremost tank end and the global reference point in x-direction.">
+                    <value>11.51890797</value>
+                    <unit>m</unit>
+                    <lower_boundary>-80</lower_boundary>
+                    <upper_boundary>80</upper_boundary>
+                </x>
+                <y description="Distance between the foremost tank end and the global reference point in y-direction.">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-40</lower_boundary>
+                    <upper_boundary>40</upper_boundary>
+                </y>
+                <z description="Distance between the foremost middle tank end and the global reference point in z-direction.">
+                    <value>-1.030445071</value>
+                    <unit>m</unit>
+                    <lower_boundary>-5</lower_boundary>
+                    <upper_boundary>5</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of all tanks.">
+                <mass description="Total tank mass.">
+                    <value>0.0</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of all tanks with regard to the total center of gravity.">
+                    <j_xx description="Inertia of all tanks in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of all tanks in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of all tanks in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of all tanks in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of all tanks in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of all tanks in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of all tanks in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of all tanks in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of all tanks in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of all tanks.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point.">
+                        <value>0.0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-80</lower_boundary>
+                        <upper_boundary>80</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point.">
+                        <value>0.0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-40</lower_boundary>
+                        <upper_boundary>40</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point.">
+                        <value>0.0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-5</lower_boundary>
+                        <upper_boundary>5</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <specific description="Tank design specific output parameter.">
+                <additional_fuselage_length description="Additional fuselage length (if smaller than 0: shrink fuselage, if greater than 0: stretch fuselage).">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </additional_fuselage_length>
+                <tank ID="0" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_0</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_inner_left</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>1.224584347</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>-1.983993414</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>1.106851328</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>-2.627613113</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.366654661</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.461678581e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>True</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8265944344420982</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.4491686948</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>1.800268099</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.291672336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-3.333830058</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5045956352728944</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.6363939604000004</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="1" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_1</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_outer_left</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>3.024852446</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>-5.317823472</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.291672336</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>0.751239882</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>-6.934994391</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.229172626</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.355603786e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>True</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5045956352728944</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.6363939604000004</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>4.742640471</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>1.057589192</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-9.092176528</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.19595492134103498</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.7427500670062859</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="2" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_2</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_inner_right</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>1.224584347</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>1.983993414</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>1.106851328</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>2.627613113</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.366654661</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.461678581e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>True</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8265944344420982</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.4491686948</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>1.800268099</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.291672336</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>3.333830058</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5045956352728944</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.6363939604000004</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="3" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_3</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_outer_right</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>3.024852446</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>5.317823472</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.291672336</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>0.751239882</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>6.934994391</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.229172626</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>1.355603786e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>True</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.5045956352728944</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.6363939604000004</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>4.742640471</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>1.057589192</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>9.092176528</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.19595492134103498</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>0.7427500670062859</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="4" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_4</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>wing_center</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>1.224584347</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>1.224584347</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>2.437021622e+11</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>True</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.98207674</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8265944344420982</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.4491686948</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-0.98207674</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.8265944344420982</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>2.4491686948</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="5" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_5</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>fuselage_center</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>6.222921737</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>-0.234554929</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>300</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>7.002921737</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>-1.2488340970274752</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>0.78</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>-1.248834097</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>9.91892625e+10</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>False</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>6.222921737</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>-0.007054929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>1.22</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.695</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.56</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>6.222921737</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>-0.234554929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.765</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>1.15</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.56</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="2" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_2</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>6.222921737</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>-0.234554929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>1.15</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.56</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="3" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_3</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>6.222921737</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>-0.234554929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-0.765</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>1.15</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.56</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="4" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_4</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>6.222921737</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>-0.007054929</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-1.22</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.695</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.56</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+                <tank ID="6" description="Description of one tank.">
+                    <name description="Name of the tank.">
+                        <value>tank_6</value>
+                    </name>
+                    <designator description="Designator of the tank.">
+                        <value>horizontal_stabilizer_total</value>
+                    </designator>
+                    <position description="Local reference point, position of one tank wrt. the tank reference point.">
+                        <x description="Distance between the foremost tank end of one tank and the tank reference point in x-direction.">
+                            <value>22.18808671</value>
+                            <unit>m</unit>
+                            <lower_boundary>-80</lower_boundary>
+                            <upper_boundary>80</upper_boundary>
+                        </x>
+                        <y description="Distance between the foremost tank end of one tank and the tank reference point in y-direction.">
+                            <value>0.0</value>
+                            <unit>m</unit>
+                            <lower_boundary>-40</lower_boundary>
+                            <upper_boundary>40</upper_boundary>
+                        </y>
+                        <z description="Distance between the foremost tank end of one tank and the tank reference point in z-direction.">
+                            <value>1.367822365</value>
+                            <unit>m</unit>
+                            <lower_boundary>-5</lower_boundary>
+                            <upper_boundary>5</upper_boundary>
+                        </z>
+                    </position>
+                    <direction description="Unit vector according to global coordinate system for direction applied at position.">
+                        <x description="X component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </x>
+                        <y description="Y component of the unit vector.">
+                            <value>1</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </y>
+                        <z description="Z component of the unit vector.">
+                            <value>0</value>
+                            <unit>m</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>1</upper_boundary>
+                        </z>
+                    </direction>
+                    <mass_properties description="Mass properties of one tank.">
+                        <mass description="Total dry mass of one tank.">
+                            <value>0.0</value>
+                            <unit>kg</unit>
+                            <lower_boundary>0</lower_boundary>
+                            <upper_boundary>inf</upper_boundary>
+                        </mass>
+                        <inertia description="Inertia of one tank with regard to its center of gravity.">
+                            <j_xx description="Inertia of the of one tank in x.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xx>
+                            <j_yy description="Inertia of the of one tank in y.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yy>
+                            <j_zz description="Inertia of the of one tank in z.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zz>
+                            <j_xy description="Inertia of one tank in xy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xy>
+                            <j_xz description="Inertia of one tank in xz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_xz>
+                            <j_yx description="Inertia of one tank in yx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yx>
+                            <j_yz description="Inertia of one tank in yz.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_yz>
+                            <j_zx description="Inertia of one tank in zx.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zx>
+                            <j_zy description="Inertia of one tank in zy.">
+                                <value>0.0</value>
+                                <unit>kgm^2</unit>
+                                <lower_boundary>-inf</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </j_zy>
+                        </inertia>
+                        <center_of_gravity description="Center of gravity of one tank.">
+                            <x description="Center of gravity in x-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Center of gravity in y-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Center of gravity in z-direction with regard to the global reference point.">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </center_of_gravity>
+                        <centroid description="Centroid of one tank.">
+                            <x description="Centroid in x-direction with regard to the local reference point.">
+                                <value>0.78</value>
+                                <unit>m</unit>
+                                <lower_boundary>-80</lower_boundary>
+                                <upper_boundary>80</upper_boundary>
+                            </x>
+                            <y description="Centroid in y-direction with regard to the local reference point.">
+                                <value>0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-40</lower_boundary>
+                                <upper_boundary>40</upper_boundary>
+                            </y>
+                            <z description="Centroid in z-direction with regard to the local reference point.">
+                                <value>0.575</value>
+                                <unit>m</unit>
+                                <lower_boundary>-5</lower_boundary>
+                                <upper_boundary>5</upper_boundary>
+                            </z>
+                        </centroid>
+                    </mass_properties>
+                    <maximum_energy_capacity description="Maximum energy capacity of one tank.">
+                        <value>7.87640829e+10</value>
+                        <unit>J</unit>
+                        <lower_boundary>0</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </maximum_energy_capacity>
+                    <energy_capacity_required_for_mission description="Energy amount required for mission.">
+                        <value>False</value>
+                    </energy_capacity_required_for_mission>
+                    <geometry description="Geometrical description of one tank.">
+                        <cross_section ID="0" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_0</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.711215719</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.010503343</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>5.539480797</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.34146778173167264</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.2723956019461944</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="1" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_1</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.646046987</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.3467541562458756</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.2920939747999998</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                        <cross_section ID="2" description="Geometrical description of one tank cross section.">
+                            <name description="Name of tank cross section.">
+                                <value>tank_section_2</value>
+                            </name>
+                            <position description="Position of tank cross section with regard to the local reference point.">
+                                <x description="Distance between the tank cross section and the local reference point in x-direction.">
+                                    <value>0.711215719</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-80</lower_boundary>
+                                    <upper_boundary>80</upper_boundary>
+                                </x>
+                                <y description="Distance between the tank cross section and the local reference point in y-direction.">
+                                    <value>0.010503343</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-40</lower_boundary>
+                                    <upper_boundary>40</upper_boundary>
+                                </y>
+                                <z description="Distance between the tank cross section and the local reference point in z-direction.">
+                                    <value>-5.539480797</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-5</lower_boundary>
+                                    <upper_boundary>5</upper_boundary>
+                                </z>
+                            </position>
+                            <shape description="Description of the shape of the cross section (circular, rectangular, elliptical).">
+                                <value>rectangular</value>
+                            </shape>
+                            <height description="Height of the cross section.">
+                                <value>0.34146778173167264</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </height>
+                            <width description="Width of the cross section.">
+                                <value>1.2723956019461944</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </width>
+                            <length description="Length of the cross section (if length greater than 0: curved cross section, e.g., dashed tank end cap).">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>inf</upper_boundary>
+                            </length>
+                        </cross_section>
+                    </geometry>
+                </tank>
+            </specific>
+        </tank>
+        <landing_gear description="Geometric description of the aircraft undercarriage." tool_level="3">
+            <position description="Position of the total undercarriage arrangement with regard to the global reference point.">
+                <x description="Distance in x direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-100</lower_boundary>
+                    <upper_boundary>100</upper_boundary>
+                </x>
+                <y description="Distance in y direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-25</lower_boundary>
+                    <upper_boundary>25</upper_boundary>
+                </y>
+                <z description="Distance in z direction with regard to the global reference point. (total undercarriage arrangement)">
+                    <value>0.0</value>
+                    <unit>m</unit>
+                    <lower_boundary>-10</lower_boundary>
+                    <upper_boundary>10</upper_boundary>
+                </z>
+            </position>
+            <mass_properties description="Mass properties of the total undercarriage arrangement.">
+                <mass description="Mass of the total undercarriage arrangement.">
+                    <value>2567.3427</value>
+                    <unit>kg</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>inf</upper_boundary>
+                </mass>
+                <inertia description="Inertia of the total undercarriage arrangement with regard to the total center of gravity.">
+                    <j_xx description="Inertia of the total undercarriage arrangement in x.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xx>
+                    <j_yy description="Inertia of the total undercarriage arrangement in y.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yy>
+                    <j_zz description="Inertia of the total undercarriage arrangement in z.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zz>
+                    <j_xy description="Inertia of the total undercarriage arrangement in xy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xy>
+                    <j_xz description="Inertia of the total undercarriage arrangement in xz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_xz>
+                    <j_yx description="Inertia of the total undercarriage arrangement in yx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yx>
+                    <j_yz description="Inertia of the total undercarriage arrangement in yz.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_yz>
+                    <j_zx description="Inertia of the total undercarriage arrangement in zx.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zx>
+                    <j_zy description="Inertia of the total undercarriage arrangement in zy.">
+                        <value>0.0</value>
+                        <unit>kgm^2</unit>
+                        <lower_boundary>-inf</lower_boundary>
+                        <upper_boundary>inf</upper_boundary>
+                    </j_zy>
+                </inertia>
+                <center_of_gravity description="Center of gravity of the total undercarriage arrangement.">
+                    <x description="Center of gravity in x-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>15.0496</value>
+                        <unit>m</unit>
+                        <lower_boundary>-100</lower_boundary>
+                        <upper_boundary>100</upper_boundary>
+                    </x>
+                    <y description="Center of gravity in y-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>0</value>
+                        <unit>m</unit>
+                        <lower_boundary>-50</lower_boundary>
+                        <upper_boundary>50</upper_boundary>
+                    </y>
+                    <z description="Center of gravity in z-direction with regard to the global reference point. (total undercarriage arrangement)">
+                        <value>-1.5763</value>
+                        <unit>m</unit>
+                        <lower_boundary>-10</lower_boundary>
+                        <upper_boundary>10</upper_boundary>
+                    </z>
+                </center_of_gravity>
+            </mass_properties>
+            <aircraft_classification_number description="Aircraft classification number for the total undercarriage arrangement. (CBR = [3, 6, 10, 15])">
+                <value>[54.8, 49.0, 44.6, 42.7]</value>
+            </aircraft_classification_number>
+            <specific description="Landing gear specific output parameter.">
+                <geometry description="Geometry description of the entire landing gear.">
+                    <landing_gear_assembly ID="0" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>nose_gear_assembly</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>6.2</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>0.0</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-1.4712</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>383.0185</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>-9.2172</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>0.0</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.1051</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2248</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>0.7352</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS01203</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.3372</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-0.7352</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>0.7699</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.2248</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS01203</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.3372</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-0.7352</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>0.7699</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.2248</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                    <landing_gear_assembly ID="1" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>right_main_gear_outer_strut</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>16.6658</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>2.8704</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-0.953</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>1092.1621</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.9895</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>2.8704</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.2566</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2322</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>1.2534</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-1.2534</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-1.2534</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                    <landing_gear_assembly ID="2" description="Geometrical description of one entire landing gear leg.">
+                        <name description="Name of the landing gear leg.">
+                            <value>left_main_gear_outer_strut</value>
+                        </name>
+                        <position description="Position of one entire landing gear leg with regard to the landing gear global position.">
+                            <x description="Distance in x direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>16.6658</value>
+                                <unit>m</unit>
+                                <lower_boundary>-100</lower_boundary>
+                                <upper_boundary>100</upper_boundary>
+                            </x>
+                            <y description="Distance in y direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-2.8704</value>
+                                <unit>m</unit>
+                                <lower_boundary>-50</lower_boundary>
+                                <upper_boundary>50</upper_boundary>
+                            </y>
+                            <z description="Distance in z direction with regard to the landing gear global position. (center line of the landing gear leg)">
+                                <value>-0.953</value>
+                                <unit>m</unit>
+                                <lower_boundary>-10</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </z>
+                        </position>
+                        <mass_properties description="Mass properties of one entire landing gear leg.">
+                            <mass description="Mass of one entire landing gear leg.">
+                                <value>1092.1621</value>
+                                <unit>kg</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10000</upper_boundary>
+                            </mass>
+                            <inertia description="Inertia of one entire landing gear leg with regard to his center of gravity.">
+                                <j_xx description="Inertia of one entire landing gear leg in x.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xx>
+                                <j_yy description="Inertia of one entire landing gear leg in y.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yy>
+                                <j_zz description="Inertia of one entire landing gear leg in z.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zz>
+                                <j_xy description="Inertia of one entire landing gear leg in xy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xy>
+                                <j_xz description="Inertia of one entire landing gear leg in xz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_xz>
+                                <j_yx description="Inertia of one entire landing gear leg in yx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yx>
+                                <j_yz description="Inertia of one entire landing gear leg in yz.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_yz>
+                                <j_zx description="Inertia of one entire landing gear leg in zx.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zx>
+                                <j_zy description="Inertia of one entire landing gear leg in zy.">
+                                    <value>0.0</value>
+                                    <unit>kgm^2</unit>
+                                    <lower_boundary>-inf</lower_boundary>
+                                    <upper_boundary>inf</upper_boundary>
+                                </j_zy>
+                            </inertia>
+                            <center_of_gravity description="Center of gravity of one entire landing gear leg.">
+                                <x description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.9895</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-100</lower_boundary>
+                                    <upper_boundary>100</upper_boundary>
+                                </x>
+                                <y description="Center of gravity in x-direction with regard to the global landing gear enter of gravity position. (entire landing gear leg)">
+                                    <value>2.8704</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-50</lower_boundary>
+                                    <upper_boundary>50</upper_boundary>
+                                </y>
+                                <z description="Center of gravity in x-direction with regard to the global landing gear center of gravity position. (entire landing gear leg)">
+                                    <value>0.2566</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>-10</lower_boundary>
+                                    <upper_boundary>10</upper_boundary>
+                                </z>
+                            </center_of_gravity>
+                        </mass_properties>
+                        <assembly_components description="Geometrical description of the assembly components of one landing gear strut.">
+                            <strut_diameter description="Diameter of the landing gear strut">
+                                <value>0.2322</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>1.0</upper_boundary>
+                            </strut_diameter>
+                            <strut_length description="Length of the landing gear strut">
+                                <value>1.2534</value>
+                                <unit>m</unit>
+                                <lower_boundary>0</lower_boundary>
+                                <upper_boundary>10</upper_boundary>
+                            </strut_length>
+                            <tire_description ID="0" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>-0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-1.2534</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                            <tire_description ID="1" description="Description of one tire of the wheel group.">
+                                <name description="Name of the tire type.">
+                                    <value>APS00524-E</value>
+                                </name>
+                                <position description="Position of one tire of current landing gear strut with regard to the landing gear strut position.">
+                                    <x description="Distance in x direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>0.0</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </x>
+                                    <y description="Distance in y direction with regard to the landing gear strut position. (center line of the landing gear strut">
+                                        <value>0.4635</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </y>
+                                    <z description="Distance in z direction with regard to the landing gear strut position. (center line of the landing gear strut)">
+                                        <value>-1.2534</value>
+                                        <unit>m</unit>
+                                        <lower_boundary>-10</lower_boundary>
+                                        <upper_boundary>10</upper_boundary>
+                                    </z>
+                                </position>
+                                <tire_diameter description="Diameter of one tire of the wheel group.">
+                                    <value>1.1493</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>2</upper_boundary>
+                                </tire_diameter>
+                                <tire_section_width description="Width at the shoulder of a tire of the wheel group.">
+                                    <value>0.4064</value>
+                                    <unit>m</unit>
+                                    <lower_boundary>0</lower_boundary>
+                                    <upper_boundary>1</upper_boundary>
+                                </tire_section_width>
+                            </tire_description>
+                        </assembly_components>
+                    </landing_gear_assembly>
+                </geometry>
+            </specific>
+        </landing_gear>
+    </component_design>
+    <sizing_point>
+        <thrust_to_weight description="Total thrust (kN) divided by maximum aircraft weight (kN)">
+            <value>0.3185737265</value>
+            <unit>1</unit>
+            <lower_boundary>0</lower_boundary>
+            <upper_boundary>1</upper_boundary>
+        </thrust_to_weight>
+        <wing_loading description="Maximum takeoff mass (MTOM) divided by wing area (Sref)">
+            <value>647.4483091</value>
+            <unit>kg/m^2</unit>
+            <lower_boundary>0</lower_boundary>
+            <upper_boundary>inf</upper_boundary>
+        </wing_loading>
+    </sizing_point>
+    <assessment description="Assessment data">
+        <performance description="Assessment of performance values">
+            <takeoff description="Takeoff assessment">
+                <takeoff_distance_normal_safety description="Takeoff distance at Sea Level for MTOM and (ISA + deltaISA)-Conditions(calculated by mission_analysis using missionDesign.xml settings) with all engines operating (AEO)">
+                    <value>1552.301412</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </takeoff_distance_normal_safety>
+            </takeoff>
+            <landing description="Landing assessment">
+                <needed_runway_length description="Needed runway length with all engines operating and maximum landing mass">
+                    <value>1288.31792</value>
+                    <unit>m</unit>
+                    <lower_boundary>0</lower_boundary>
+                    <upper_boundary>5000</upper_boundary>
+                </needed_runway_length>
+            </landing>
+        </performance>
+    </assessment>
+</aircraft_exchange_file>
diff --git a/projects/oldFormat-CSR.xml b/projects/oldFormat-CSR.xml
new file mode 100644
index 0000000000000000000000000000000000000000..6b4c8683fbe9007cce157f079ec5ee5b10ec17e7
--- /dev/null
+++ b/projects/oldFormat-CSR.xml
@@ -0,0 +1,3866 @@
+<AcftExchangeFile>
+    <General Desc="Allgemeine Angaben">
+        <Type Desc="Flugzeugtyp" Unit="-">CeRAS</Type>
+        <Model Desc="Modell bzw. Ausfuehrung" Unit="-">CSR-01</Model>
+    </General>
+    <MassesAndLoadings Desc="-">
+        <MassBreakdown Desc="Massenverteilung">
+            <Wing Desc="Fluegelmasse und Schwerpunktlage des Massenelements, Airbus Chapter 10">
+                <Mass ToolLevel="1" Unit="kg">8535.455741</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                    <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                </RefPoint>
+                <CenterWing Desc="Masse der Fluegelstruktur (Skins, Spars, Ribs, Pylon attachments, LG supports), Airbus Ch. 10.0-4">
+                    <Mass ToolLevel="1" Unit="kg">6278.799947</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                        <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                    </RefPoint>
+                    <EoW_CenterWingMassFactor Desc="Center wing mass factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_CenterWingMassFactor>
+                    <EoW_AeroelasticFactor Desc="Aeroelastic (flutter) factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_AeroelasticFactor>
+                    <EoW_TotalCenterWingMassFactor Desc="EoW_CenterWingMassFactor * EoW_AeroelasticFactor" ToolLevel="1" Unit="-">1</EoW_TotalCenterWingMassFactor>
+                </CenterWing>
+                <WingLEandTE Desc="Masse der Hochauftriebssysteme, Airbus Ch. 10.5-8">
+                    <Mass ToolLevel="1" Unit="kg">2256.655794</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                        <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                    </RefPoint>
+                    <FixedLeadingEdge Desc="Mass of the complete fixed leading edge, Airbus Ch. 10.5">
+                        <Mass ToolLevel="1" Unit="kg">291.6450898</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                            <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                        </RefPoint>
+                    </FixedLeadingEdge>
+                    <MovableLeadingEdge Desc="Mass of the complete movable leading edge, Airbus Ch. 10.6">
+                        <Mass ToolLevel="1" Unit="kg">373.9546469</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                            <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                        </RefPoint>
+                    </MovableLeadingEdge>
+                    <FixedTrailingEdge Desc="Mass of the fixed trailing edge, Airbus Ch. 10.7">
+                        <Mass ToolLevel="1" Unit="kg">582.2672595</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                            <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                        </RefPoint>
+                    </FixedTrailingEdge>
+                    <MovableTrailingEdge Desc="Mass of the movable trailing edge, Airbus Ch. 10.8">
+                        <Mass ToolLevel="1" Unit="kg">1008.788798</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                            <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                        </RefPoint>
+                    </MovableTrailingEdge>
+                </WingLEandTE>
+                <Miscellaneous Desc="Restliche Fluegelmassenanteile, Airbus Ch. 10.9">
+                    <Mass ToolLevel="1" Unit="kg">0</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                        <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                    </RefPoint>
+                </Miscellaneous>
+            </Wing>
+            <Fuselage Desc="Rumpfmasse und Schwerpunktlage des Massenelements, Airbus Chapter 11">
+                <Mass Desc="-" ToolLevel="1" Unit="kg">8888.102165</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                    <y_Item Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                </RefPoint>
+            </Fuselage>
+            <Empennage Desc="Masse der Leitwerksgruppe und Schwerpunktlage des Massenelements">
+                <Mass Desc="Gesamtmasse der Leitwerksgruppe" ToolLevel="1" Unit="kg">1257.118042</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.40806564</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
+                </RefPoint>
+                <Tailplane Desc="Airbus Chapter 13">
+                    <Mass ToolLevel="1" Unit="kg">705.5278242</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">33.73963722</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
+                    </RefPoint>
+                </Tailplane>
+                <Fin Desc="Airbus Chapter 14">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">551.5902181</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">32.98395918</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Item>
+                    </RefPoint>
+                </Fin>
+            </Empennage>
+            <LandingGear Desc="Fahrwerksmasse und Schwerpunktlage des Massenelements, Airbus Chapter 15">
+                <Mass Desc="-" ToolLevel="1" Unit="kg">2518.773274</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.32982807</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.469648031</h_Item>
+                </RefPoint>
+                <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
+                    <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">377.8159911</TotalMass>
+                    <RefPoint Desc="Position of NoseGear CofG to global point of reference">
+                        <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                    <Strut>
+                        <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+                        <RefPoint Desc="position of strut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Strut>
+                    <SupportStrut>
+                        <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+                        <RefPoint Desc="position of suppStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </SupportStrut>
+                    <WheelGroupConnection>
+                        <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+                        <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </WheelGroupConnection>
+                    <WheelGroup>
+                        <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+                        <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+                        <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+                        <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+                    </WheelGroup>
+                </Gear>
+                <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
+                    <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass>
+                    <RefPoint Desc="Position of OuterRightMainGear CofG to global point of reference">
+                        <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                    <Strut>
+                        <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+                        <RefPoint Desc="position of strut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Strut>
+                    <SupportStrut>
+                        <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+                        <RefPoint Desc="position of suppStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </SupportStrut>
+                    <WheelGroupConnection>
+                        <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+                        <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </WheelGroupConnection>
+                    <WheelGroup>
+                        <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+                        <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+                        <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+                        <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+                    </WheelGroup>
+                </Gear>
+                <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
+                    <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">1070.478642</TotalMass>
+                    <RefPoint Desc="Position of OuterLeftMainGear CofG to global point of reference">
+                        <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                    <Strut>
+                        <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+                        <RefPoint Desc="position of strut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Strut>
+                    <SupportStrut>
+                        <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+                        <RefPoint Desc="position of suppStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </SupportStrut>
+                    <WheelGroupConnection>
+                        <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+                        <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </WheelGroupConnection>
+                    <WheelGroup>
+                        <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+                        <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+                        <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+                        <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+                    </WheelGroup>
+                </Gear>
+                <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
+                    <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass>
+                    <RefPoint Desc="Position of InnerRightMainGear CofG to global point of reference">
+                        <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                    <Strut>
+                        <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+                        <RefPoint Desc="position of strut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Strut>
+                    <SupportStrut>
+                        <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+                        <RefPoint Desc="position of suppStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </SupportStrut>
+                    <WheelGroupConnection>
+                        <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+                        <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </WheelGroupConnection>
+                    <WheelGroup>
+                        <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+                        <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+                        <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+                        <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+                    </WheelGroup>
+                </Gear>
+                <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
+                    <TotalMass Desc="Mass of single gear" ToolLevel="1" Unit="kg">0</TotalMass>
+                    <RefPoint Desc="Position of InnerLeftMainGear CofG to global point of reference">
+                        <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                    <Strut>
+                        <strutMass Desc="strut mass" ToolLevel="1" Unit="kg">0</strutMass>
+                        <RefPoint Desc="position of strut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Strut>
+                    <SupportStrut>
+                        <suppStrutMass Desc="Mass of support strut" ToolLevel="1" Unit="kg">0</suppStrutMass>
+                        <RefPoint Desc="position of suppStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </SupportStrut>
+                    <WheelGroupConnection>
+                        <connStrutMass Desc="Mass of connection strut" ToolLevel="1" Unit="kg">0</connStrutMass>
+                        <RefPoint Desc="position of wheelGroupConnectionStrut CofG to global point of reference">
+                            <r_Item Desc="Position of CofG in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of CofG in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of CofG in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </WheelGroupConnection>
+                    <WheelGroup>
+                        <tiresMass Desc="Overall mass of tires" ToolLevel="1" Unit="kg">0</tiresMass>
+                        <axesMass Desc="Overall mass of axes" ToolLevel="1" Unit="kg">0</axesMass>
+                        <rimMass Desc="Rim mass" ToolLevel="1" Unit="kg">0</rimMass>
+                        <brakeMass Desc="brake mass" ToolLevel="1" Unit="kg">0</brakeMass>
+                    </WheelGroup>
+                </Gear>
+            </LandingGear>
+            <Pylons Desc="Pylonmasse und Schwerpunktlage (aller Pylons), Airbus Chapter 16">
+                <Mass Desc="-" ToolLevel="1" Unit="kg">1049.543431</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.59758377</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.838904205</h_Item>
+                </RefPoint>
+            </Pylons>
+            <PowerUnit Desc="Masse und Schwerpunktlage der Triebwerksanlage, Airbus Group Power Unit">
+                <Mass Desc="Gesamtmasse der Gruppe Antriebsanlage" ToolLevel="1" Unit="kg">7983.304178</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.56488425</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.882731847</h_Item>
+                </RefPoint>
+                <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="1">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">3749.798796</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                    </RefPoint>
+                    <EngineDry Desc="Engine dry mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">2237.636365</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                        </RefPoint>
+                    </EngineDry>
+                    <Nacelle Desc="Nacelle mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                        </RefPoint>
+                    </Nacelle>
+                    <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">5.219203967</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                        </RefPoint>
+                    </OtherSystems>
+                    <Prop Desc="Propeller mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Prop>
+                </Engine>
+                <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="2">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">3749.798796</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                    </RefPoint>
+                    <EngineDry Desc="Engine dry mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                        </RefPoint>
+                    </EngineDry>
+                    <Nacelle Desc="Nacelle mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">1069.077788</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                        </RefPoint>
+                    </Nacelle>
+                    <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">443.0846426</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.4373365</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">-5.219203967</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-2.992711155</h_Item>
+                        </RefPoint>
+                    </OtherSystems>
+                    <Prop Desc="Propeller mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Prop>
+                </Engine>
+                <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="3">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                    <EngineDry Desc="Engine dry mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </EngineDry>
+                    <Nacelle Desc="Nacelle mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Nacelle>
+                    <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </OtherSystems>
+                    <Prop Desc="Propeller mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Prop>
+                </Engine>
+                <Engine Desc="Ausruestmasse eines Triebwerks, Airbus Chapter 20" ID="4">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                    <EngineDry Desc="Engine dry mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </EngineDry>
+                    <Nacelle Desc="Nacelle mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Nacelle>
+                    <OtherSystems Desc="Other systems mass eg. hydraulics, starter, etc.">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </OtherSystems>
+                    <Prop Desc="Propeller mass">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Prop>
+                </Engine>
+                <BleedAirSystem Desc="Airbus Chapter 21, ATA36">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">170.4663501</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
+                    </RefPoint>
+                </BleedAirSystem>
+                <EngineControls Desc="Airbus Chapter 22">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </EngineControls>
+                <FuelSystem Desc="Airbus Chapter 25, ATA28">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">313.2402355</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.92875025</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.09429915</h_Item>
+                    </RefPoint>
+                </FuelSystem>
+            </PowerUnit>
+            <Systems Desc="Systemmasse und Schwerpunktlage des Massenelements, Airbus Group Systems">
+                <Mass Desc="Gesamtmasse der Systemgruppe" ToolLevel="1" Unit="kg">5309.46001</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.22640698</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-0.5973844066</h_Item>
+                </RefPoint>
+                <APU Desc="Airbus Chapter 30, ATA49">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">269.6524446</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">35.12321805</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </APU>
+                <HydraulicGeneration Desc="Airbus Chapter 31, ATA 29">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">177.4943728</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
+                    </RefPoint>
+                </HydraulicGeneration>
+                <HydraulicDistribution Desc="Airbus Chapter 32, ATA 29">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">795.934215</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
+                    </RefPoint>
+                </HydraulicDistribution>
+                <AirConditioning Desc="Airbus Chapter 33, ATA21">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">711.2165166</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
+                    </RefPoint>
+                </AirConditioning>
+                <DeIcing Desc="Airbus Chapter 34, ATA30">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">41.98276817</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </DeIcing>
+                <FireProtection Desc="Airbus Chapter 35, ATA26">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">92.36094204</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </FireProtection>
+                <FlightControls Desc="Airbus Chapter 36, ATA27">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">699.137886</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83257644</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Item>
+                    </RefPoint>
+                    <Roll Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.0">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">42.43977661</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Roll>
+                    <Yaw Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.1">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">97.75474213</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Yaw>
+                    <Pitch Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.2">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">30.4466164</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Pitch>
+                    <MovableHorizontalTail Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.3">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">63.38988998</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </MovableHorizontalTail>
+                    <Flaps Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.4">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">143.8595475</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Flaps>
+                    <SpoilersAirbrakesLiftdumpers Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.5">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">38.76193929</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </SpoilersAirbrakesLiftdumpers>
+                    <Slats Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.6">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">142.6577969</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </Slats>
+                    <CommonInstallation Desc="Mass of the aileron actuators, their installations and operation controls, Airbus Ch. 36.7">
+                        <Mass Desc="-" ToolLevel="1" Unit="kg">139.8275772</Mass>
+                        <RefPoint Desc="position of mass item to global point of reference">
+                            <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                            <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                            <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                        </RefPoint>
+                    </CommonInstallation>
+                </FlightControls>
+                <Instruments Desc="Airbus Chapter 37, ATA31">
+                    <Mass ToolLevel="1" Unit="kg">85.16128872</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">4.34075992</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </Instruments>
+                <AutomaticFlightSystem Desc="Airbus Chapter 38, ATA 22">
+                    <Mass ToolLevel="1" Unit="kg">138.3870942</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </AutomaticFlightSystem>
+                <Navigation Desc="Airbus Chapter 39, ATA34">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">564.1935378</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </Navigation>
+                <Communication Desc="Airbus Chapter 40, ATA23">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">276.7741884</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </Communication>
+                <ElectricalGeneration Desc="Airbus Chapter 41, ATA24">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">774.2507101</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </ElectricalGeneration>
+                <ElectricalDistribution Desc="Airbus Chapter 42, ATA24">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">682.914046</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </ElectricalDistribution>
+            </Systems>
+            <Furnishings Desc="Furnishingmasse und Schwerpunktlage des Massenelements, Airbus Group Furnishings">
+                <Mass Desc="Gesamtmasse der Furnishinggruppe" ToolLevel="1" Unit="kg">3114.623325</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                </RefPoint>
+                <Furnishing Desc="Airbus Chapter 50, ATA25">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">2464.223172</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </Furnishing>
+                <FixedEmergencyOxygen Desc="Airbus Chapter 51, ATA35">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">98.464</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </FixedEmergencyOxygen>
+                <Lighting Desc="Airbus Chapter 52, ATA33">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">261.9261532</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </Lighting>
+                <WaterInstallation Desc="Airbus Chapter 53, ATA38">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">290.01</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.63731381</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </WaterInstallation>
+            </Furnishings>
+            <OperatorsItems Desc="Masse der Betreiberausstattung und Schwerpunktlage des Massenelements, Airbus Group Operator Items">
+                <Mass Desc="Gesamtmasse der Operators Items Gruppe" ToolLevel="1" Unit="kg">3326.415065</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">14.54754916</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                </RefPoint>
+                <OperatorEquipment Desc="Airbus Chapter 60 (fixed equipment, vorher Standard Items)">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">1575.865065</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.5703719</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </OperatorEquipment>
+                <OperationalEquipment Desc="Airbus Chapter 61  (movable equipment)">
+                    <Mass Desc="-" ToolLevel="1" Unit="kg">1750.55</Mass>
+                    <RefPoint Desc="position of mass item to global point of reference">
+                        <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">12.72658107</r_Item>
+                        <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                        <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                    </RefPoint>
+                </OperationalEquipment>
+            </OperatorsItems>
+            <NotAllocated Desc="Nicht zugeordnete Massenanteile und Schwerpunktlage des Massenelements">
+                <Mass Desc="-" ToolLevel="1" Unit="kg">0</Mass>
+                <RefPoint Desc="position of mass item to global point of reference">
+                    <r_Item Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Item>
+                    <y_Item Desc="Position of reference in y-direction" ToolLevel="1" Unit="m">0</y_Item>
+                    <h_Item Desc="Position of reference in z-direction" ToolLevel="1" Unit="m">0</h_Item>
+                </RefPoint>
+            </NotAllocated>
+        </MassBreakdown>
+        <MTM Desc="Maximum Taxi Mass" ToolLevel="1" Unit="kg">0</MTM>
+        <MLM Desc="Maximum Landing Mass" ToolLevel="1" Unit="kg">65025.01668</MLM>
+        <MTOM Desc="Maximum Take-Off Mass" ToolLevel="3" Unit="kg">80000</MTOM>
+        <MRM Desc="Maximum Ramp Mass" ToolLevel="1" Unit="kg">0</MRM>
+        <MME Desc="Manufacturing Mass Empty" ToolLevel="1" Unit="kg">38656.38017</MME>
+        <OME Desc="Operating Mass Empty" ToolLevel="1" Unit="kg">999</OME>
+        <MZFM Desc="Maximum Zero Fuel Mass" ToolLevel="1" Unit="kg">61982.79523</MZFM>
+        <MaximumPayload Desc="Maximale Nutzlast" ToolLevel="1" Unit="kg">20000</MaximumPayload>
+        <MaximumUsableFuel Desc="Benutzbare Kraftstoffmasse" ToolLevel="1" Unit="kg">31084.34394</MaximumUsableFuel>
+        <WingLoading Desc="Fluegelflaechenlast" ToolLevel="1" Unit="kg/m2">628.681385</WingLoading>
+        <ThrustToWeight Desc="Schubkraft (kN) zu Gewichtskrafthaeltnis (kN)" ToolLevel="1" Unit="-">0.3218120393</ThrustToWeight>
+        <PowerToWeight Desc="Leistungsgewicht" ToolLevel="1" Unit="kW/kg">0</PowerToWeight>
+        <MomentsOfInertia Desc="Flaechentraegheitsmomente">
+            <Ixx Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixx>
+            <Iyy Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyy>
+            <Izz Desc="-" ToolLevel="1" Unit="kg*m2">0</Izz>
+            <Ixy Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixy>
+            <Ixz Desc="-" ToolLevel="1" Unit="kg*m2">0</Ixz>
+            <Iyz Desc="-" ToolLevel="1" Unit="kg*m2">0</Iyz>
+        </MomentsOfInertia>
+        <CentreOfGravityRange Desc="Schwerpunktsgrenzen">
+            <TrimRefPt Desc="Schwerpunktlage fuer CM-Berechnung und Trimmung im Reiseflug">
+                <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.7359472859</h>
+                <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.56950713</r>
+                <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
+            </TrimRefPt>
+            <ForwardLimit Desc="Vorderste Schwerpunktlage">
+                <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-0.9505895064</h>
+                <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.4584795</r>
+                <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
+            </ForwardLimit>
+            <AftLimit Desc="Hinterste Schwerpunktlage">
+                <h Desc="Position of the COG in reference to the global point of reference in z-direction" ToolLevel="1" Unit="m">-1.011726725</h>
+                <r Desc="Position of the COG in reference to the global point of reference in x-direction" ToolLevel="1" Unit="m">16.65854294</r>
+                <y Desc="Position of the COG in reference to the global point of reference in y-direction" ToolLevel="1" Unit="m">0</y>
+            </AftLimit>
+        </CentreOfGravityRange>
+    </MassesAndLoadings>
+    <Geometry Desc="Geometriebeschreibung">
+        <UsedElements Desc="Liste der verwendeten Geometrieelemente">
+            <LiftingSurfaces Desc="Anzahl der verwendeten Elemente LiftingSurface" ToolLevel="1">2</LiftingSurfaces>
+            <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="1" ToolLevel="1" Unit="-">MainWing</LiftingSurface>
+            <LiftingSurface Desc="Name des verwendeten LiftingSurface-Elements" ID="2" ToolLevel="1" Unit="-">Stabiliser</LiftingSurface>
+            <VerticalSurfaces Desc="Anzahl der verwendeten Elemente VerticalSurface" ToolLevel="1">1</VerticalSurfaces>
+            <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="1" ToolLevel="1" Unit="-">Fin</VerticalSurface>
+            <VerticalSurface Desc="Name des verwendeten VerticalSurface-Elements" ID="2" ToolLevel="1" Unit="-">0</VerticalSurface>
+            <Fuselages Desc="Anzahl der verwendeten Elemente Fuselage" ToolLevel="1">1</Fuselages>
+            <Fuselage Desc="Name des verwendeten Fuselage-Elements" ID="1" ToolLevel="1" Unit="-">Fuselage</Fuselage>
+            <Nacelles Desc="Anzahl der verwendeten Elemente Nacelle" ToolLevel="1">2</Nacelles>
+            <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingNacelle</Nacelle>
+            <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingNacelle</Nacelle>
+            <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="3" ToolLevel="1" Unit="-">0</Nacelle>
+            <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="4" ToolLevel="1" Unit="-">0</Nacelle>
+            <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="5" ToolLevel="1" Unit="-">0</Nacelle>
+            <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="6" ToolLevel="1" Unit="-">0</Nacelle>
+            <Nacelle Desc="Name des verwendeten Nacelle-Elements" ID="7" ToolLevel="1" Unit="-">0</Nacelle>
+            <Pylons Desc="Anzahl der verwendeten Elemente Pylon" ToolLevel="1">2</Pylons>
+            <Pylon Desc="Name des verwendeten Pylon-Elements" ID="1" ToolLevel="1" Unit="-">InnerRightWingPylon</Pylon>
+            <Pylon Desc="Name des verwendeten Pylon-Elements" ID="2" ToolLevel="1" Unit="-">InnerLeftWingPylon</Pylon>
+            <Pylon Desc="Name des verwendeten Pylon-Elements" ID="3" ToolLevel="1" Unit="-">0</Pylon>
+            <Pylon Desc="Name des verwendeten Pylon-Elements" ID="4" ToolLevel="1" Unit="-">0</Pylon>
+            <Pylon Desc="Name des verwendeten Pylon-Elements" ID="5" ToolLevel="1" Unit="-">0</Pylon>
+            <Pylon Desc="Name des verwendeten Pylon-Elements" ID="6" ToolLevel="1" Unit="-">0</Pylon>
+            <Gears Desc="Anzahl der verwendeten Elemente Gear" ToolLevel="1">3</Gears>
+            <Gear Desc="Name des verwendeten Gear-Elements" ID="1" ToolLevel="1" Unit="-">NoseGear</Gear>
+            <Gear Desc="Name des verwendeten Gear-Elements" ID="2" ToolLevel="1" Unit="-">OuterRightMainGear</Gear>
+            <Gear Desc="Name des verwendeten Gear-Elements" ID="3" ToolLevel="1" Unit="-">OuterLeftMainGear</Gear>
+            <Gear Desc="Name des verwendeten Gear-Elements" ID="4" ToolLevel="1" Unit="-">0</Gear>
+            <Gear Desc="Name des verwendeten Gear-Elements" ID="5" ToolLevel="1" Unit="-">0</Gear>
+        </UsedElements>
+        <LiftingSurface Desc="Beschreibung des Hauptfluegels" ID="MainWing">
+            <SurfaceRefPoint Desc="position of wing to global point of reference">
+                <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">12.34780307</r_Surface>
+                <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
+                <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330569364</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of lifting surface geometry">
+                <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
+                <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
+                <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">0</i_Surface>
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">200</SectionPoints>
+                <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
+                    <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">2</HalfSurfaceSegments>
+                    <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
+                        <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_15.dat</InnerProfile_Segment>
+                        <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</OuterProfile_Segment>
+                        <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">6.969546741</l_i_Segment>
+                        <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">4.363049953</l_o_Segment>
+                        <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">5.115537999</s_Segment>
+                        <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                        <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.091406079</nu_Segment>
+                        <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
+                        <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.11</l_rel_i_FrontSpar>
+                        <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.55</l_rel_i_RearSpar>
+                        <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.16</l_rel_o_FrontSpar>
+                        <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.65</l_rel_o_RearSpar>
+                    </HalfSurfaceSegment>
+                    <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="Surface">
+                        <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_12.dat</InnerProfile_Segment>
+                        <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">F15_11.dat</OuterProfile_Segment>
+                        <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">4.363049953</l_i_Segment>
+                        <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.036840684</l_o_Segment>
+                        <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">11.93625533</s_Segment>
+                        <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                        <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">2.374274265</nu_Segment>
+                        <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">26.99999996</phi_Segment>
+                        <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.16</l_rel_i_FrontSpar>
+                        <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
+                        <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.27</l_rel_o_FrontSpar>
+                        <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
+                    </HalfSurfaceSegment>
+                    <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
+                        <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                        <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                        <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                        <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                        <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+                        <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                        <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                        <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                        <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+                        <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+                        <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+                        <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+                    </HalfSurfaceSegment>
+                    <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+                        <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">8</TEDevices>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.2</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Fowler</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.78</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">45</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">Aileron</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.8</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.98</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerGround</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2062430536</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.125</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.25</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.294</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.306</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.4195</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.4195</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.533</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.533</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.6465</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">SpoilerAir</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.6465</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.15</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0.3</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.76</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.15</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0.3</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">40</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">1</LEDevices>
+                        <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+                            <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">Slat</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.1184861071</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.11</l_rel_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.27</l_rel_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">35</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </LEDevice>
+                    </ControlDeviceSetup>
+                </HalfSurfaceDescription>
+                <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
+                    <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
+                    <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
+                        <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                        <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                        <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                        <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                        <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+                        <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                        <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                        <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                        <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+                        <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+                        <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+                        <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+                    </HalfSurfaceSegment>
+                    <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+                        <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
+                        <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+                            <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </LEDevice>
+                    </ControlDeviceSetup>
+                </HalfSurfaceDescription>
+            </SurfaceParameters>
+        </LiftingSurface>
+        <LiftingSurface Desc="Beschreibung des Hoehenleitwerks" ID="Stabiliser">
+            <SurfaceRefPoint Desc="position of wing to global point of reference">
+                <r_Surface Desc="Position of the wing to global point of reference in x-direction" ToolLevel="1" Unit="m">31.1606612</r_Surface>
+                <y_Surface Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Surface>
+                <h_Surface Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">1.692105859</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of lifting surface geometry">
+                <Symmetric Desc="1:= symmetric wing / 0 := asymmetric wing" ToolLevel="1" Unit="-">1</Symmetric>
+                <RelChordRefForRotation Desc="Rel. Chordtiefe: Ref.-Pkt. fuer Verwindg. u. V-Stellg." ToolLevel="1" Unit="-">0</RelChordRefForRotation>
+                <i_Surface Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="deg">-1.140234056</i_Surface>
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <HalfSurfaceDescription Desc="Parameters of right wing (or both wings, if symmetric)" ID="1">
+                    <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">1</HalfSurfaceSegments>
+                    <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
+                        <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
+                        <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
+                        <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.962556849</l_i_Segment>
+                        <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.11563951</l_o_Segment>
+                        <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">6.392179667</s_Segment>
+                        <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                        <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                        <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">31.99999988</phi_Segment>
+                        <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.15</l_rel_i_FrontSpar>
+                        <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0.65</l_rel_i_RearSpar>
+                        <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.3</l_rel_o_FrontSpar>
+                        <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0.55</l_rel_o_RearSpar>
+                    </HalfSurfaceSegment>
+                    <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
+                        <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                        <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                        <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                        <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                        <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+                        <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                        <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                        <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                        <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+                        <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+                        <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+                        <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+                    </HalfSurfaceSegment>
+                    <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+                        <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+                            <Type Desc="Typ der Hinterkantenflaeche (Elevator)" ToolLevel="1">Elevator</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
+                        <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+                            <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </LEDevice>
+                    </ControlDeviceSetup>
+                </HalfSurfaceDescription>
+                <HalfSurfaceDescription Desc="Parameters of left wing (if asymmetric)" ID="2">
+                    <HalfSurfaceSegments Desc="Number of wing segments in this half surface" ToolLevel="1" Unit="-">0</HalfSurfaceSegments>
+                    <HalfSurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="0">
+                        <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                        <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                        <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                        <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                        <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+                        <epsilon_Segment Desc="Angle of twist of wing segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                        <nu_Segment Desc="Angle of dihedral of wing segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                        <phi_Segment Desc="Leading edge sweep angle of wing segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                        <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+                        <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+                        <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+                        <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+                    </HalfSurfaceSegment>
+                    <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+                        <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">0</TEDevices>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="2">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="3">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="4">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="5">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="6">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="7">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="8">
+                            <Type Desc="Typ der Hinterkantenflaeche (Aileron, DroopAileron, Flap, SlottedFlap, Fowler, DoubleFowler, TripleFowler, Special, SpoilerGround, SpoilerAir, morphingTrailingEdge)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <l_rel_TE_i Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device innen" ToolLevel="1" Unit="-">0</l_rel_TE_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <l_rel_TE_o Desc="relative Sehnentiefe von Hinterkante Fluegel zu Hinterkante device aussen" ToolLevel="1" Unit="-">0</l_rel_TE_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </TEDevice>
+                        <LEDevices Desc="Anzahl der Vorderkantenflaechen" ToolLevel="1">0</LEDevices>
+                        <LEDevice Desc="Beschreibung eines Vorderkantenelements" ID="1">
+                            <Type Desc="Typ der Vorderkantenflaeche (Slat, Krueger, DroopNose, morphingDroopNose, Special)" ToolLevel="1">0</Type>
+                            <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0</s_rel_i>
+                            <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0</l_rel_i>
+                            <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0</s_rel_o>
+                            <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0</l_rel_o>
+                            <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                                <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullPos>
+                                <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">0</FullNeg>
+                            </DeflectionAngle>
+                        </LEDevice>
+                    </ControlDeviceSetup>
+                </HalfSurfaceDescription>
+            </SurfaceParameters>
+        </LiftingSurface>
+        <VerticalSurface Desc="Beschreibung des Seitenleitwerks" ID="Fin">
+            <SurfaceRefPoint Desc="Referenzpunkt der vertikalen Steuerflaeche">
+                <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">29.20843962</r_Surface>
+                <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+                <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">1.692105859</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of vertical surface geometry">
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <SurfaceSegments Desc="Number of segments in this vertical surface" ToolLevel="1">1</SurfaceSegments>
+                <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="1" Type="Surface">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">5.914778427</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">1.564960467</l_o_Segment>
+                    <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">7.105751949</s_Segment>
+                    <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">38.99999987</phi_Segment>
+                    <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+                    <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+                    <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+                    <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="2" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                    <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+                    <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+                    <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+                    <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung (verfuegbare Typen: Fuselage, Surface, Tip)" ID="3" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of wing segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <phi_Segment Desc="Angle of dsweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                    <l_rel_i_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_FrontSpar>
+                    <l_rel_i_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante innen" ToolLevel="1" Unit="-">0</l_rel_i_RearSpar>
+                    <l_rel_o_FrontSpar Desc="rel. Sehnentiefe des Vorderholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_FrontSpar>
+                    <l_rel_o_RearSpar Desc="rel. Sehnentiefe des Hinterholmes von der Vorderkante aussen" ToolLevel="1" Unit="-">0</l_rel_o_RearSpar>
+                </SurfaceSegment>
+                <ControlDeviceSetup Desc="Planformbeschreibung der Steuerflaechen">
+                    <TEDevices Desc="Anzahl der Hinterkantenflaechen" ToolLevel="1">1</TEDevices>
+                    <TEDevice Desc="Beschreibung eines Hinterkantenelements" ID="1">
+                        <Type Desc="Typ der Hinterkantenflaeche (Rudder)" ToolLevel="1">Rudder</Type>
+                        <s_rel_i Desc="relative Spannweite innen" ToolLevel="1" Unit="-">0.2</s_rel_i>
+                        <l_rel_i Desc="relative Sehnentiefe innen" ToolLevel="1" Unit="-">0.3</l_rel_i>
+                        <s_rel_o Desc="relative Spannweite aussen" ToolLevel="1" Unit="-">0.95</s_rel_o>
+                        <l_rel_o Desc="relative Sehnentiefe aussen" ToolLevel="1" Unit="-">0.3</l_rel_o>
+                        <DeflectionAngle Desc="Steuerflaechenausschlagwinkel">
+                            <FullPos Desc="Maximaler Ausschlagwinkel in positive Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">20</FullPos>
+                            <FullNeg Desc="Maximaler Ausschlagwinkel in negative Richtung (Winkeldef.)" ToolLevel="1" Unit="deg">-20</FullNeg>
+                        </DeflectionAngle>
+                    </TEDevice>
+                </ControlDeviceSetup>
+            </SurfaceParameters>
+        </VerticalSurface>
+        <Fuselage Desc="Beschreibung des Rumpfes" ID="Fuselage">
+            <FuselageRefPoint Desc="position of the fuselage nose refpoint to global point of reference">
+                <r_Fuselage Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Fuselage>
+                <y_Fuselage Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Fuselage>
+                <h_Fuselage Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Fuselage>
+            </FuselageRefPoint>
+            <FuselageParameters Desc="parametric description of the fuselage">
+                <NoseDescription>
+                    <NoseSegments Desc="No of nose segments" ToolLevel="1">9</NoseSegments>
+                    <TipSegment>
+                        <h_Tip Desc="offset of nosetip" ToolLevel="1" Unit="m">-0.5351396212</h_Tip>
+                    </TipSegment>
+                    <NoseSegment ID="1">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.6205763694</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.6626671728</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.06782437376</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.5351396212</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="2">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.229534829</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.312928447</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.2034731213</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.4376004301</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="3">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.814885649</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.937980885</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.3391218688</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.3438425644</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="4">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.363843474</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.524171961</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.4747706164</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.2559139029</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="5">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">2.862283086</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.05641841</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.6104193639</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1760769356</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="6">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.293963779</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.517377993</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.7460681114</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.1069329983</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="7">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.639314251</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.886151978</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0.8817168589</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.05161690045</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="8">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.873337327</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.136047749</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.017365606</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0.01413253478</deltah_Segment>
+                    </NoseSegment>
+                    <NoseSegment ID="9">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.230264648</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.153014354</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">-0</deltah_Segment>
+                    </NoseSegment>
+                </NoseDescription>
+                <MidSectionDescription>
+                    <MidSectionSegments Desc="No of mid-segment segments" ToolLevel="1">1</MidSectionSegments>
+                    <MidSectionSegment ID="1">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.230264648</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">15.57908662</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
+                    </MidSectionSegment>
+                    <MidSectionSegment ID="2">
+                        <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0</deltah_Segment>
+                    </MidSectionSegment>
+                </MidSectionDescription>
+                <TailDescription>
+                    <TailSegments Desc="No of tail segments" ToolLevel="1">7</TailSegments>
+                    <TailSegment ID="1">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">4.163206861</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.0335288931</deltah_Segment>
+                    </TailSegment>
+                    <TailSegment ID="2">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.961569826</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.960934992</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.1346648278</deltah_Segment>
+                    </TailSegment>
+                    <TailSegment ID="3">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.893957495</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.620061515</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.3051015662</deltah_Segment>
+                    </TailSegment>
+                    <TailSegment ID="4">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.614493823</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">3.151622366</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.539321141</deltah_Segment>
+                    </TailSegment>
+                    <TailSegment ID="5">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">3.115516897</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">2.662987184</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">1.823611325</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">0.7836387319</deltah_Segment>
+                    </TailSegment>
+                    <TailSegment ID="6">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">1.980784913</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">1.754520057</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.390445476</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.237872295</deltah_Segment>
+                    </TailSegment>
+                    <TailSegment ID="7">
+                        <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                        <w_Segment Desc="Breite des Rumpf-Segments" ToolLevel="1" Unit="m">0.8460529295</w_Segment>
+                        <h_Segment Desc="Hoehe des Rumpf-Segments" ToolLevel="1" Unit="m">0.8460529295</h_Segment>
+                        <l_Segment Desc="Laenge des Rumpf-Segments" ToolLevel="1" Unit="m">3.390445476</l_Segment>
+                        <deltah_Segment Desc="Verticales Offset des Rumpf-Segments" ToolLevel="1" Unit="m">1.692105859</deltah_Segment>
+                    </TailSegment>
+                </TailDescription>
+            </FuselageParameters>
+        </Fuselage>
+        <Nacelle Desc="Beschreibung der inneren rechten Triebwerksgondel" ID="InnerRightWingNacelle">
+            <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+                <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.1833365</r_Nacelle>
+                <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">5.219203967</y_Nacelle>
+                <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Nacelle>
+            </NacelleRefPoint>
+            <NacelleParameters Desc="parametric description of the nacelle">
+                <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+                <Points Desc="No of points describing the section" ToolLevel="1">20</Points>
+                <Segments Desc="No of segments" ToolLevel="1">2</Segments>
+                <InletSegment>
+                    <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                    <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Inlet>
+                    <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Inlet>
+                    <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Inlet>
+                </InletSegment>
+                <NacelleSegment ID="1">
+                    <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.254</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="2">
+                    <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="3">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="4">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <ExitSegment>
+                    <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                    <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Exit>
+                    <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Exit>
+                </ExitSegment>
+            </NacelleParameters>
+            <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+        </Nacelle>
+        <Nacelle Desc="Beschreibung der inneren linken Triebwerksgondel" ID="InnerLeftWingNacelle">
+            <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+                <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.1833365</r_Nacelle>
+                <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-5.219203967</y_Nacelle>
+                <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Nacelle>
+            </NacelleRefPoint>
+            <NacelleParameters Desc="parametric description of the nacelle">
+                <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+                <Points Desc="No of points describing the section" ToolLevel="1">20</Points>
+                <Segments Desc="No of segments" ToolLevel="1">2</Segments>
+                <InletSegment>
+                    <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                    <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Inlet>
+                    <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Inlet>
+                    <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Inlet>
+                </InletSegment>
+                <NacelleSegment ID="1">
+                    <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">1.254</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="2">
+                    <InnerSegmentPointData ToolLevel="1">fuselage.dat</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">fuselage.dat</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">2.28625</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.6475</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0.627</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="3">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="4">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <ExitSegment>
+                    <SegmentPointData ToolLevel="1">fuselage.dat</SegmentPointData>
+                    <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">2.118</h_Exit>
+                    <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">1.829</w_Exit>
+                </ExitSegment>
+            </NacelleParameters>
+            <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+        </Nacelle>
+        <Nacelle Desc="Beschreibung der aeusseren rechten Triebwerksgondel" ID="OuterRightWingNacelle">
+            <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+                <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+                <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+                <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+            </NacelleRefPoint>
+            <NacelleParameters Desc="parametric description of the nacelle">
+                <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+                <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+                <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+                <InletSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+                    <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+                    <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+                </InletSegment>
+                <NacelleSegment ID="1">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="2">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <ExitSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+                    <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+                </ExitSegment>
+            </NacelleParameters>
+            <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+        </Nacelle>
+        <Nacelle Desc="Beschreibung der aeusseren linken Triebwerksgondel" ID="OuterLeftWingNacelle">
+            <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+                <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+                <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+                <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+            </NacelleRefPoint>
+            <NacelleParameters Desc="parametric description of the nacelle">
+                <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+                <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+                <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+                <InletSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+                    <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+                    <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+                </InletSegment>
+                <NacelleSegment ID="1">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="2">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <ExitSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+                    <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+                </ExitSegment>
+            </NacelleParameters>
+            <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+        </Nacelle>
+        <Nacelle Desc="Beschreibung der rechten Hecktriebwerksgondel" ID="RightFuselageNacelle">
+            <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+                <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+                <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+                <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+            </NacelleRefPoint>
+            <NacelleParameters Desc="parametric description of the nacelle">
+                <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+                <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+                <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+                <InletSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+                    <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+                    <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+                </InletSegment>
+                <NacelleSegment ID="1">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="2">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <ExitSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+                    <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+                </ExitSegment>
+            </NacelleParameters>
+            <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+        </Nacelle>
+        <Nacelle Desc="Beschreibung der linken Hecktriebwerksgondel" ID="LeftFuselageNacelle">
+            <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+                <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+                <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+                <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+            </NacelleRefPoint>
+            <NacelleParameters Desc="parametric description of the nacelle">
+                <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+                <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+                <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+                <InletSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+                    <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+                    <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+                </InletSegment>
+                <NacelleSegment ID="1">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="2">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <ExitSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+                    <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+                </ExitSegment>
+            </NacelleParameters>
+            <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+        </Nacelle>
+        <Nacelle Desc="Beschreibung der in das SLW integrierten Triebwerksgondel" ID="FinNacelle">
+            <NacelleRefPoint Desc="Referenzpunkt der Nacelle. Mittelpunkt des Einlaufs">
+                <r_Nacelle Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Nacelle>
+                <y_Nacelle Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Nacelle>
+                <h_Nacelle Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Nacelle>
+            </NacelleRefPoint>
+            <NacelleParameters Desc="parametric description of the nacelle">
+                <i_Nacelle Desc="Angle of incidence in reference to the aircrafts coordinate system" ToolLevel="1" Unit="degree">0</i_Nacelle>
+                <Points Desc="No of points describing the section" ToolLevel="1">0</Points>
+                <Segments Desc="No of segments" ToolLevel="1">0</Segments>
+                <InletSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <w_Inlet Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Inlet>
+                    <h_Inlet Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Inlet>
+                    <l_Inlet Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Inlet>
+                </InletSegment>
+                <NacelleSegment ID="1">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <NacelleSegment ID="2">
+                    <InnerSegmentPointData ToolLevel="1">0</InnerSegmentPointData>
+                    <OuterSegmentPointData ToolLevel="1">0</OuterSegmentPointData>
+                    <w_i_Segment Desc="Innere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_i_Segment>
+                    <w_o_Segment Desc="aeussere Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_o_Segment>
+                    <h_i_Segment Desc="Innere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_i_Segment>
+                    <h_o_Segment Desc="aeussere Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_o_Segment>
+                    <l_Segment Desc="Laenge des Nacelle-Segments" ToolLevel="1" Unit="m">0</l_Segment>
+                </NacelleSegment>
+                <ExitSegment>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <h_Exit Desc="Hoehe des Nacelle-Segments" ToolLevel="1" Unit="m">0</h_Exit>
+                    <w_Exit Desc="Breite des Nacelle-Segments" ToolLevel="1" Unit="m">0</w_Exit>
+                </ExitSegment>
+            </NacelleParameters>
+            <EngineTypeID Desc="Angabe der EngineType ID zwecks Zuordnung des korrekten Motors in dieser Nacelle" ToolLevel="1">0</EngineTypeID>
+        </Nacelle>
+        <Pylon Desc="Beschreibung des Pylons" ID="InnerRightWingPylon">
+            <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+                <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface>
+                <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">5.219203967</y_Surface>
+                <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of pylon geometry">
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+            </SurfaceParameters>
+        </Pylon>
+        <Pylon Desc="Beschreibung des Pylons" ID="InnerLeftWingPylon">
+            <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+                <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">13.4341365</r_Surface>
+                <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">-5.219203967</y_Surface>
+                <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.992711155</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of pylon geometry">
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">2</SurfaceSegments>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="Surface">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.0096</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">3.762</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">1.11195</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="Surface">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">n0012.dat</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">3.762</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">2.11583452</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0.7413</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">71.91922836</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+            </SurfaceParameters>
+        </Pylon>
+        <Pylon Desc="Beschreibung des Pylons" ID="OuterRightWingPylon">
+            <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+                <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+                <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+                <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of pylon geometry">
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+            </SurfaceParameters>
+        </Pylon>
+        <Pylon Desc="Beschreibung des Pylons" ID="OuterLeftWingPylon">
+            <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+                <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+                <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+                <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of pylon geometry">
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+            </SurfaceParameters>
+        </Pylon>
+        <Pylon Desc="Beschreibung des Pylons" ID="RightFuselagePylon">
+            <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+                <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+                <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+                <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of pylon geometry">
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+            </SurfaceParameters>
+        </Pylon>
+        <Pylon Desc="Beschreibung des Pylons" ID="LeftFuselagePylon">
+            <SurfaceRefPoint Desc="Referenzpunkt des Pylons">
+                <r_Surface Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Surface>
+                <y_Surface Desc="Seitenlage in y-Richtung - i.d.R. = 0 !" ToolLevel="1" Unit="m">0</y_Surface>
+                <h_Surface Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Surface>
+            </SurfaceRefPoint>
+            <SurfaceParameters Desc="Parametric description of pylon geometry">
+                <SectionPoints Desc="number of points of profile. Will be used by spline interpolation if DoInterpolate attribute is set true" DoInterpolate="0" ToolLevel="1" Unit="-">0</SectionPoints>
+                <SurfaceSegments Desc="Number of segments in this pylon" ToolLevel="1">0</SurfaceSegments>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="1" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="2" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+                <SurfaceSegment Desc="Segmentbeschreibung" ID="3" Type="0">
+                    <InnerProfile_Segment Desc="Inner airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</InnerProfile_Segment>
+                    <OuterProfile_Segment Desc="Outer airfoil segment. Geometry is stored in seperate file (*.dat)" ToolLevel="1">0</OuterProfile_Segment>
+                    <l_i_Segment Desc="Chord length of segments inner profile" ToolLevel="1" Unit="m">0</l_i_Segment>
+                    <l_o_Segment Desc="Chord length of segments outer profile" ToolLevel="1" Unit="m">0</l_o_Segment>
+                    <s_Segment Desc="Span of surface segment" ToolLevel="1" Unit="m">0</s_Segment>
+                    <epsilon_Segment Desc="Angle of twist of surface segment" ToolLevel="1" Unit="deg">0</epsilon_Segment>
+                    <nu_Segment Desc="Angle of dihedral of surface segment" ToolLevel="1" Unit="deg">0</nu_Segment>
+                    <phi_Segment Desc="Angle of sweep of surface segment" ToolLevel="1" Unit="deg">0</phi_Segment>
+                </SurfaceSegment>
+            </SurfaceParameters>
+        </Pylon>
+        <Gear Desc="Beschreibung des Bugfahrwerks" ID="NoseGear">
+            <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+                <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Gear>
+                <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
+                <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-2.023847396</h_Gear>
+            </GearRefPoint>
+            <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+                <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">3.662516183</r_Wheelgroup>
+                <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
+                <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.834540304</h_Wheelgroup>
+            </WheelGroupRefPoint>
+            <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.127127</StrutDiameter>
+            <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
+            <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+                <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+                <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+                <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+            </HingeAxis>
+            <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
+            <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+            <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.3911791258</Wheeltrack>
+            <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
+            <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
+            <Wheel Desc="Beschreibung des Rades">
+                <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0.6858</TireDiameter>
+                <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.19558</TireWidth>
+                <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.3429</RimDiameter>
+            </Wheel>
+        </Gear>
+        <Gear Desc="Beschreibung des aeusseren, rechten Hauptfahrwerks" ID="OuterRightMainGear">
+            <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+                <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear>
+                <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Gear>
+                <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear>
+            </GearRefPoint>
+            <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+                <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup>
+                <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">4.076078967</y_Wheelgroup>
+                <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup>
+            </WheelGroupRefPoint>
+            <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
+            <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
+            <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+                <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+                <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+                <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+            </HingeAxis>
+            <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">-90</RetractionAngle>
+            <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+            <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
+            <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
+            <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
+            <Wheel Desc="Beschreibung des Rades">
+                <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
+                <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
+                <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
+            </Wheel>
+        </Gear>
+        <Gear Desc="Beschreibung des aeusseren, linken Hauptfahrwerks" ID="OuterLeftMainGear">
+            <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+                <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.63676778</r_Gear>
+                <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Gear>
+                <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-1.371848143</h_Gear>
+            </GearRefPoint>
+            <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+                <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">17.5474552</r_Wheelgroup>
+                <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">-4.076078967</y_Wheelgroup>
+                <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">-4.593240304</h_Wheelgroup>
+            </WheelGroupRefPoint>
+            <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0.32385</StrutDiameter>
+            <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">1</Retractable>
+            <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+                <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+                <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+                <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+            </HingeAxis>
+            <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">90</RetractionAngle>
+            <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+            <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0.8636932256</Wheeltrack>
+            <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">1</NumberOfAxes>
+            <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">2</NumberOfWheelsPerAxis>
+            <Wheel Desc="Beschreibung des Rades">
+                <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">1.1684</TireDiameter>
+                <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0.4318</TireWidth>
+                <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0.5842</RimDiameter>
+            </Wheel>
+        </Gear>
+        <Gear Desc="Beschreibung des inneren, rechten Hauptfahrwerks" ID="InnerRightMainGear">
+            <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+                <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
+                <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
+                <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
+            </GearRefPoint>
+            <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+                <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
+                <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
+                <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
+            </WheelGroupRefPoint>
+            <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
+            <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
+            <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+                <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+                <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+                <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+            </HingeAxis>
+            <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
+            <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+            <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
+            <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
+            <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
+            <Wheel Desc="Beschreibung des Rades">
+                <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
+                <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
+                <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
+            </Wheel>
+        </Gear>
+        <Gear Desc="Beschreibung des inneren, linken Hauptfahrwerks" ID="InnerLeftMainGear">
+            <GearRefPoint Desc="Referenzpunkt. Aufhaengungs- bzw. Drehpunkt des Fahrwerks">
+                <r_Gear Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Gear>
+                <y_Gear Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Gear>
+                <h_Gear Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Gear>
+            </GearRefPoint>
+            <WheelGroupRefPoint Desc="Referenzpunkt der Radgruppe. Endpunkt des Fahrwerksbeins auf Achshoehe in der Mitte der Achsen.">
+                <r_Wheelgroup Desc="Ruecklage in x Richtung" ToolLevel="1" Unit="m">0</r_Wheelgroup>
+                <y_Wheelgroup Desc="Seitenlage in y-Richtung" ToolLevel="1" Unit="m">0</y_Wheelgroup>
+                <h_Wheelgroup Desc="Hochlage in z-Richtung" ToolLevel="1" Unit="m">0</h_Wheelgroup>
+            </WheelGroupRefPoint>
+            <StrutDiameter Desc="Durchmesser des Fahrwerkbeins" ToolLevel="1" Unit="m">0</StrutDiameter>
+            <Retractable Desc="Fahrwerk einziehbar = 1, festes Fahrwerk = 0" ToolLevel="1">0</Retractable>
+            <HingeAxis Desc="Drehachse als Einheitsvektor um die das Fahrwerks einfaehrt (Im Math. Sinne positiv)">
+                <x Desc="x-Komponente des Vektors" ToolLevel="1" Unit="-">0</x>
+                <y Desc="y-Komponente des Vektors" ToolLevel="1" Unit="-">0</y>
+                <z Desc="z-Komponente des Vektors" ToolLevel="1" Unit="-">0</z>
+            </HingeAxis>
+            <RetractionAngle Desc="Winkel um den das Fahrwerk zum Einziehen gedreht wird" ToolLevel="1" Unit="deg">0</RetractionAngle>
+            <Wheelbase Desc="Abstand der vordersten zur hintersten Achse der Radgruppe, Radstand" ToolLevel="1" Unit="m">0</Wheelbase>
+            <Wheeltrack Desc="Spurweite der Radgruppe" ToolLevel="1" Unit="m">0</Wheeltrack>
+            <NumberOfAxes Desc="Achsenzahl der Radgruppe hintereinander. Abstand wird gleichmaessig auf Radstand verteilt" ToolLevel="1">0</NumberOfAxes>
+            <NumberOfWheelsPerAxis Desc="Anzahl der Raeder pro Achse" ToolLevel="1">0</NumberOfWheelsPerAxis>
+            <Wheel Desc="Beschreibung des Rades">
+                <TireDiameter Desc="Reifendurchmesser" ToolLevel="1" Unit="m">0</TireDiameter>
+                <TireWidth Desc="Reifenbreite" ToolLevel="1" Unit="m">0</TireWidth>
+                <RimDiameter Desc="Felgendurchmesser" ToolLevel="1" Unit="m">0</RimDiameter>
+            </Wheel>
+        </Gear>
+    </Geometry>
+    <Structure Desc="Strukturdaten"></Structure>
+    <Accommodation Desc="Kabineneinrichtung">
+        <PassengersTotal Desc="Gesamtanzahl der Sitzplaetze" ToolLevel="1">150</PassengersTotal>
+        <FlightCrew Desc="Anzahl Cockpitbesatzung" ToolLevel="1">2</FlightCrew>
+        <CabinCrew Desc="Anzahl Flugbegleiter" ToolLevel="1">4</CabinCrew>
+        <Seats Desc="Description of seats">
+            <NoOfSeatTypes Desc="Anzahl der Sitzklassen" ToolLevel="1">5</NoOfSeatTypes>
+            <seat Desc="Description of seat" ID="1">
+                <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">commuter</seatClassType>
+                <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">1</noOfSeatConfigurations>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="5">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">0</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">0</noOfSeats>
+                </seatConfiguration>
+                <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
+                <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE>
+            </seat>
+            <seat Desc="Description of seat" ID="2">
+                <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">economy</seatClassType>
+                <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">4</noOfSeatConfigurations>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">9</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">14</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">19.5</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="4">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">4</noOfSeats>
+                </seatConfiguration>
+                <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
+                <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
+            </seat>
+            <seat Desc="Description of seat" ID="3">
+                <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">GeneralAviation</seatClassType>
+                <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">15</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">25.1</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
+                </seatConfiguration>
+                <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">0</IFE>
+                <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0</massIFE>
+            </seat>
+            <seat Desc="Description of seat" ID="4">
+                <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">business</seatClassType>
+                <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">3</noOfSeatConfigurations>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">27.2</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">35.1</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
+                </seatConfiguration>
+                <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
+                <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
+            </seat>
+            <seat Desc="Description of seat" ID="5">
+                <seatClassType Desc="Passagierklasse fuer die der Sitztyp vorgesehen ist" ToolLevel="1">first</seatClassType>
+                <noOfSeatConfigurations Desc="Anzahl der Sitzkonfigurationen" ToolLevel="1">2</noOfSeatConfigurations>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="1">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">21.25</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">1</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="2">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">42.5</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">2</noOfSeats>
+                </seatConfiguration>
+                <seatConfiguration Desc="Description of SeatConfiguration" ID="3">
+                    <mass Desc="Masse der Sitze" ToolLevel="1" Unit="kg">43</mass>
+                    <noOfSeats Desc="Anzahl der Sitze in einer Sitzgruppe" ToolLevel="1">3</noOfSeats>
+                </seatConfiguration>
+                <IFE Desc="Inflight entertainment system verbaut" ToolLevel="1">1</IFE>
+                <massIFE Desc="Masse des Passagier Unterhaltungs System pro Person" ToolLevel="1" Unit="kg">0.4</massIFE>
+            </seat>
+        </Seats>
+        <Galleys Desc="Description of galleys">
+            <NoOfGalleyTypes Desc="Anzahl verwendeter Kuechen Typen" ToolLevel="1">2</NoOfGalleyTypes>
+            <Gal Desc="Description of galley" ID="1">
+                <nameGalley Desc="Name of galley" ToolLevel="1">large_galley</nameGalley>
+                <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
+                <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">226.8</mass>
+                <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">14418</power>
+            </Gal>
+            <Gal Desc="Description of galley" ID="2">
+                <nameGalley Desc="Name of galley" ToolLevel="1">small_galley</nameGalley>
+                <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">1</NumberOfGalleys>
+                <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">61.24</mass>
+                <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">3887</power>
+            </Gal>
+            <Gal Desc="Description of galley" ID="3">
+                <nameGalley Desc="Name of galley" ToolLevel="1">0</nameGalley>
+                <NumberOfGalleys Desc="Gesamtzahl der verwendeten Galleys dieses Typs" ToolLevel="1">0</NumberOfGalleys>
+                <mass Desc="Masse der Galleystruktur" ToolLevel="1" Unit="kg">0</mass>
+                <power Desc="Leistungsabnahme der Galley" ToolLevel="1" Unit="kW">0</power>
+            </Gal>
+        </Galleys>
+        <Lavatories Desc="Description of lavatories">
+            <NoOfLavatoryTypes Desc="Anzahl verwendeter Lavatorie-Typen" ToolLevel="1">1</NoOfLavatoryTypes>
+            <Lav Desc="Description of lavatory" ID="1">
+                <nameLavatory Desc="Name of lavatory" ToolLevel="1">standard_lavatory</nameLavatory>
+                <NumberOfLavatories Desc="Gesamtzahl der verwendeten Lavatories dieses Typs" ToolLevel="1">3</NumberOfLavatories>
+                <mass Desc="Masse einer Lavatoryeinheit" ToolLevel="1" Unit="kg">96.67</mass>
+            </Lav>
+        </Lavatories>
+        <Cabin Desc="Beschreibung der Kabine">
+            <V_AirConditioned Desc="Klimatisiertes Kabinenvolumen gesamt" ToolLevel="1" Unit="m3">190.47918</V_AirConditioned>
+            <CabinDecks Desc="Anzahl Kabinendecks" ToolLevel="1">1</CabinDecks>
+            <CabinDeck Desc="Parameter eines Kabinendecks" ID="1">
+                <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">95.53300238</A_CabinDeck>
+                <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">2.13</h_CabinDeck>
+                <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">3.613074406</w_CabinDeck>
+                <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">26.44091752</l_CabinDeck>
+                <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">185.9285625</V_CabinDeck>
+                <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">150</PAX_CabinDeck>
+                <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">2</Classes>
+                <Class Desc="Definition der Klasse" ID="1">
+                    <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">6.044387137</x_center>
+                </Class>
+                <Class Desc="Definition der Klasse" ID="2">
+                    <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">19.2648459</x_center>
+                </Class>
+                <Class Desc="Definition der Klasse" ID="3">
+                    <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Class>
+            </CabinDeck>
+            <CabinDeck Desc="Parameter eines Kabinendecks" ID="2">
+                <A_CabinDeck Desc="Flaeche des Kabinendecks" ToolLevel="1" Unit="m2">0</A_CabinDeck>
+                <h_CabinDeck Desc="maximale Kabinenhoehe" ToolLevel="1" Unit="m">0</h_CabinDeck>
+                <w_CabinDeck Desc="maximale Kabinenbreite" ToolLevel="1" Unit="m">0</w_CabinDeck>
+                <l_CabinDeck Desc="Kabinenlaenge ohne Flight-Deck" ToolLevel="1" Unit="m">0</l_CabinDeck>
+                <V_CabinDeck Desc="Kabinenvolumen" ToolLevel="1" Unit="m3">0</V_CabinDeck>
+                <PAX_CabinDeck Desc="Sitzplaetze des Kabinendecks" ToolLevel="1">0</PAX_CabinDeck>
+                <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck" ToolLevel="1">0</Classes>
+                <Class Desc="Definition der Klasse" ID="1">
+                    <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Class>
+                <Class Desc="Definition der Klasse" ID="2">
+                    <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Class>
+                <Class Desc="Definition der Klasse" ID="3">
+                    <x_center Desc="Mittelpunkt der Klasse in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Class>
+            </CabinDeck>
+        </Cabin>
+        <Cargo Desc="Beschreibung des Frachtraums">
+            <V_Cargo Desc="Frachtvolumen gesamt" ToolLevel="1" Unit="m3">33.22757663</V_Cargo>
+            <CargoDecks Desc="Anzahl Frachtdecks" ToolLevel="1">1</CargoDecks>
+            <CargoDeck Desc="Parameter eines Frachtdecks" ID="1">
+                <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">55.02284727</A_CargoDeck>
+                <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">1.14</h_CargoDeck>
+                <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">3.252922327</w_CargoDeck>
+                <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">16.91489736</l_CargoDeck>
+                <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">34.30498624</V_CargoDeck>
+                <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">12.17849076</V_BulkCargo>
+                <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">2</Compartments>
+                <Compartment Desc="Definition des Compartments" ID="1">
+                    <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">4.69</Length>
+                    <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">6.045</x_center>
+                </Compartment>
+                <Compartment Desc="Definition des Compartments" ID="2">
+                    <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">6.22</Length>
+                    <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">23.42652858</x_center>
+                </Compartment>
+                <Compartment Desc="Definition des Compartments" ID="3">
+                    <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
+                    <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Compartment>
+            </CargoDeck>
+            <CargoDeck Desc="Parameter eines Frachtdecks" ID="2">
+                <A_CargoDeck Desc="Flaeche des Frachtdecks" ToolLevel="1" Unit="m2">0</A_CargoDeck>
+                <h_CargoDeck Desc="maximale Deckhoehe" ToolLevel="1" Unit="m">0</h_CargoDeck>
+                <w_CargoDeck Desc="maximale Deckbreite" ToolLevel="1" Unit="m">0</w_CargoDeck>
+                <l_CargoDeck Desc="Decklaenge" ToolLevel="1" Unit="m">0</l_CargoDeck>
+                <V_CargoDeck Desc="Deckvolumen" ToolLevel="1" Unit="m3">0</V_CargoDeck>
+                <V_BulkCargo Desc="Freies Frachtvolumen fuer Bulk-Cargo" ToolLevel="1" Unit="m3">0</V_BulkCargo>
+                <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck" ToolLevel="1">0</Compartments>
+                <Compartment Desc="Definition des Compartments" ID="1">
+                    <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
+                    <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Compartment>
+                <Compartment Desc="Definition des Compartments" ID="2">
+                    <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
+                    <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Compartment>
+                <Compartment Desc="Definition des Compartments" ID="3">
+                    <Length Desc="Laenge des Compartments" ToolLevel="1" Unit="m">0</Length>
+                    <x_center Desc="Mittelpunkt des Compartments in x-Richtung" ToolLevel="1" Unit="m">0</x_center>
+                </Compartment>
+            </CargoDeck>
+        </Cargo>
+    </Accommodation>
+    <Propulsion Desc="Angabe der verwendeten Engine Types (nicht jede einzelne Engine)">
+        <NumberOfEngineTypes Desc="Anzahl verschiedener Triebwerkstypen" ToolLevel="1">0</NumberOfEngineTypes>
+        <Engine Desc="Triebwerks-/Motortyp" ID="1">
+            <TypeOfEngine Desc="Triebwerkstyp z.Zt. Jet oder Prop" ToolLevel="1" Unit="-">jet</TypeOfEngine>
+            <EngineModel Desc="Triebwerksmodell fuer Gummimotor" ToolLevel="1" Unit="-">V2527-A5</EngineModel>
+            <NumberOfEngines Desc="Anzahl der Triebwerke - notwendig?" ToolLevel="1">2</NumberOfEngines>
+            <ScaleEngines Desc="Skalierungsfaktor fuer das Triebwerksmodell i.S.e. Gummimotors" ToolLevel="1" Unit="-">1.039876757</ScaleEngines>
+            <ScaleFuelFlow Desc="Skalierungsfaktor fuer den Fuel Flow" ToolLevel="1" Unit="-">1</ScaleFuelFlow>
+            <EngineDataFile Desc="Name der Triebewerksdatei (enthaelt Geometriedaten und Decks)" ToolLevel="1" Unit="-">V2527-A5/V2527-A5.xml</EngineDataFile>
+            <JetEngineData Desc="Jet spezifische Triebwerksdaten">
+                <SeaLevelStaticThrust Desc="Flat-Rated Standschub" ToolLevel="1" Unit="kN">121.4507148</SeaLevelStaticThrust>
+                <FanDiameter Desc="Durchmesser des Fans" ToolLevel="1" Unit="m">1.613</FanDiameter>
+            </JetEngineData>
+            <TurbopropEngineData Desc="Prop spezifische Triebwerksdaten">
+                <Prop Desc="Propellerdaten">
+                    <PropDiameter Desc="Propellerdurchmesser" ToolLevel="1" Unit="m">0</PropDiameter>
+                    <PropBlades Desc="Anzahl Propellerblaetter" ToolLevel="1">0</PropBlades>
+                    <SegmentPointData ToolLevel="1">0</SegmentPointData>
+                    <Pitch Desc="Variable oder Fix Pitch" ToolLevel="1">0</Pitch>
+                    <Thickness Desc="Thickness of rotor disc " ToolLevel="1" Unit="m">0</Thickness>
+                </Prop>
+                <P_shp Desc="Triebwerkswellenleistung" ToolLevel="1" Unit="kW">0</P_shp>
+            </TurbopropEngineData>
+            <EngineDimensions Desc="Geometrische Abmasse des skalierten Triebwerks, Kerntriebwerk">
+                <w_Engine Desc="Breite des uninstallierten Triebwerks" ToolLevel="1" Unit="m">1.829</w_Engine>
+                <h_Engine Desc="Hoehe des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.118</h_Engine>
+                <l_Engine Desc="Gesamtlaenge des uninstallierten Triebwerks" ToolLevel="1" Unit="m">2.508</l_Engine>
+            </EngineDimensions>
+            <NacelleRescaling Desc="Parameter fuer Rescaling der Wing Nacelles" Matched="0">
+                <InnerNacelle>
+                    <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
+                    <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
+                    <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
+                    <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
+                    <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
+                    <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
+                </InnerNacelle>
+                <OuterNacelle>
+                    <DeltaXPos Desc="Relative axiale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaXPos>
+                    <RelYPos Desc="Relative spannweitige Position der Nacelle" ToolLevel="1" Unit="-">0</RelYPos>
+                    <DeltaZPos Desc="Relative vertikale Position der Nacelle (bzgl. Wing-MAC)" ToolLevel="1" Unit="-">0</DeltaZPos>
+                    <WidthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-breite" ToolLevel="1" Unit="-">0</WidthRatio>
+                    <HeightRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-hoehe" ToolLevel="1" Unit="-">0</HeightRatio>
+                    <LengthRatio Desc="Referenzverhaeltnis Nacelle- zu TWs-laenge" ToolLevel="1" Unit="-">0</LengthRatio>
+                </OuterNacelle>
+            </NacelleRescaling>
+            <ScaledPerformanceCharacteristics Desc="Leistungscharakteristik des (eines!) skalierten Triebwerks">
+                <EquivalentThrust Desc="1.25 * Max-Go-Around (Schub bei ISA+15, SL, Ma0.25, N1 100 perc)" ToolLevel="1" Unit="kN">121.6192213</EquivalentThrust>
+                <MaximumTakeOff Desc="Maximale Startschubbedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0 Mach=0.0">
+                    <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">121.4507148</Thrust>
+                    <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.255306839</FuelFlow>
+                    <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01033593619</TSFC>
+                    <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.027199488</N1>
+                </MaximumTakeOff>
+                <MaximumGoAround Desc="Maximale Go-Around-Bedingung bei ISA+15 und keinen Off-takes bei Altitude_ft=0.0, Mach=0.25">
+                    <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">97.29537705</Thrust>
+                    <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">1.274976051</FuelFlow>
+                    <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01310417914</TSFC>
+                    <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1.02423458</N1>
+                </MaximumGoAround>
+                <MaximumContinous Altitude_ft="35000" Desc="Maximales Schublimit ohne Zeitlimit bei ISA+0 bei" Mach="0.78">
+                    <MaxThrust Desc="Without Offtakes">
+                        <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">35.65209987</Thrust>
+                        <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.6237266005</FuelFlow>
+                        <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01749480683</TSFC>
+                        <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">1</N1>
+                    </MaxThrust>
+                    <BucketThrust Desc="Without Offtakes">
+                        <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.92001194</Thrust>
+                        <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4343473894</FuelFlow>
+                        <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01675722181</TSFC>
+                        <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.875</N1>
+                    </BucketThrust>
+                    <BucketThrustOfftakes Desc="With Average Cruise Offtakes (s. Design Mission)">
+                        <Thrust Desc="Schubkraft" ToolLevel="1" Unit="kN">25.97268447</Thrust>
+                        <FuelFlow Desc="Treibstoffverbrauch" ToolLevel="1" Unit="kg/s">0.4521939534</FuelFlow>
+                        <TSFC Desc="Thrust specific fuel consumption" ToolLevel="1" Unit="(kg/s)/kN">0.01741036641</TSFC>
+                        <N1 Desc="Relative LP shaft rotation speed" ToolLevel="1" Unit="percent">0.905</N1>
+                    </BucketThrustOfftakes>
+                </MaximumContinous>
+            </ScaledPerformanceCharacteristics>
+            <UsedForNacelles Desc="Angabe der Nacelle IDs, in welche dieser Engine Type eingebaut wird">
+                <UsedForNumberOfEngines ToolLevel="1">0</UsedForNumberOfEngines>
+                <NacelleID ID="1" ToolLevel="1">0</NacelleID>
+                <NacelleID ID="2" ToolLevel="1">0</NacelleID>
+                <NacelleID ID="3" ToolLevel="1">0</NacelleID>
+                <NacelleID ID="4" ToolLevel="1">0</NacelleID>
+            </UsedForNacelles>
+        </Engine>
+    </Propulsion>
+    <Systems>
+        <FuelTank Desc="Tank system Parameters">
+            <CentreTanks Desc="No of centre tanks" ToolLevel="1">1</CentreTanks>
+            <CentreTank Desc="Center-Tank Beschreibung" ID="1">
+                <RefPoint Desc="position of tank reference point in relation to global point of reference">
+                    <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">15.83307738</r_Tank>
+                    <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank>
+                    <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.330577781</h_Tank>
+                </RefPoint>
+                <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">10165.96362</TankVolume>
+            </CentreTank>
+            <WingTanks Desc="No of wing tanks" ToolLevel="1">2</WingTanks>
+            <WingTank Desc="Fluegeltank-Beschreibung" ID="1">
+                <RefPoint Desc="position of tank reference point in relation to global point of reference">
+                    <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank>
+                    <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">6.308425637</y_Tank>
+                    <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank>
+                </RefPoint>
+                <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume>
+            </WingTank>
+            <WingTank Desc="Fluegeltank-Beschreibung" ID="2">
+                <RefPoint Desc="position of tank reference point in relation to global point of reference">
+                    <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">16.57026607</r_Tank>
+                    <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">-6.308425637</y_Tank>
+                    <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">-1.094307567</h_Tank>
+                </RefPoint>
+                <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">14715.96338</TankVolume>
+            </WingTank>
+            <TrimTanks Desc="No of trim tanks" ToolLevel="1">0</TrimTanks>
+            <TrimTank Desc="Trimmtank-Beschreibung" ID="1">
+                <RefPoint Desc="position of tank reference point in relation to global point of reference">
+                    <r_Tank Desc="Position of reference in x-direction" ToolLevel="1" Unit="m">0</r_Tank>
+                    <y_Tank Desc="Position of the wing to global point of reference in y-direction" ToolLevel="1" Unit="m">0</y_Tank>
+                    <h_Tank Desc="Position of the wing to global point of reference in z-direction" ToolLevel="1" Unit="m">0</h_Tank>
+                </RefPoint>
+                <TankVolume Desc="Tankvolumen" ToolLevel="1" Unit="l">0</TankVolume>
+            </TrimTank>
+            <TotalFuelVolume Desc="Gesamtes Kraftstoffvolumen aller Tanks" ToolLevel="1" Unit="l">39597.89037</TotalFuelVolume>
+        </FuelTank>
+        <ATA21_EnvironmentalControlSystem>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">25.96155032</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.315916839</BleedAir>
+            </DesignPower>
+            <AirflowPerPax Desc="Konstanter Luftmassenstrom pro Passagier" ToolLevel="1" Unit="lbs/min">0.75</AirflowPerPax>
+            <Recirculation Desc="Prozentualer Anteil der Kabinenluft, die wieder verwendet wird (0.0 - 1.0)" ToolLevel="1" Unit="-">0.4</Recirculation>
+        </ATA21_EnvironmentalControlSystem>
+        <ATA22_AutoFlight>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA22_AutoFlight>
+        <ATA23_Communication>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA23_Communication>
+        <ATA24_ElectricSystem>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA24_ElectricSystem>
+        <ATA25_Furnishing>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">18.92</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA25_Furnishing>
+        <ATA26_FireProtection>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA26_FireProtection>
+        <ATA27_FlightControlSystem>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">95.17958985</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA27_FlightControlSystem>
+        <ATA28_FuelSystem>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">11.89508876</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA28_FuelSystem>
+        <ATA29_HydraulicSystem>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">7.171489811</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+            <Pressure Desc="Nenn-Druck des Hydrauliksystems" ToolLevel="1" Unit="psi">3000</Pressure>
+        </ATA29_HydraulicSystem>
+        <ATA30_IceRainProtection>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">14.0269</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">1.128183366</BleedAir>
+            </DesignPower>
+        </ATA30_IceRainProtection>
+        <ATA31_Instrumentation>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA31_Instrumentation>
+        <ATA32_LandingGear>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">67.03267969</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA32_LandingGear>
+        <ATA33_Lights>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">7.96874401</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA33_Lights>
+        <ATA34_Navigation>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA34_Navigation>
+        <ATA35_Oxygen>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0</BleedAir>
+            </DesignPower>
+        </ATA35_Oxygen>
+        <ATA36_BleedAir>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">0.1286368529</BleedAir>
+            </DesignPower>
+        </ATA36_BleedAir>
+        <ATA49_APU>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">0</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">0</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-0</BleedAir>
+            </DesignPower>
+        </ATA49_APU>
+        <ATA70_PropulsionSystem>
+            <DesignPower Desc="Maximaler Energiebedarf fuer Auslegung">
+                <Electric Desc="Maximaler Bedarf an elektrischer Energie" ToolLevel="1" Unit="kW">-142.0813445</Electric>
+                <Hydraulic Desc="Maximaler Bedarf an hydraulischer Energie" ToolLevel="1" Unit="kW">-174.2129642</Hydraulic>
+                <BleedAir Desc="Maximaler Bedarf an Bleed Air" ToolLevel="1" Unit="kg/s">-2.708144271</BleedAir>
+            </DesignPower>
+        </ATA70_PropulsionSystem>
+    </Systems>
+    <Aerodynamics Desc="Aerodynamik">
+        <LoverD_Cruise Desc="Beste Gleitzahl L/D im Reiseflug fuer (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">17.07161371</LoverD_Cruise>
+        <LiftCoefficients Desc="Auftriebsbeiwerte">
+            <C_L_design Desc="Design Auftriebsbeiwert" ToolLevel="1" Unit="-">0.5388392246</C_L_design>
+            <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert Landekonfiguration" ToolLevel="1" Unit="-">2.910828613</C_LmaxLanding>
+            <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert Startkonfiguration" ToolLevel="1" Unit="-">2.511580029</C_LmaxT-O>
+            <C_LoptimumCruise Desc="Auftriebsbeiwert bei bestem LoverD bei (Initial) Cruise Machzahl" ToolLevel="1" Unit="-">0.534</C_LoptimumCruise>
+            <C_L_opt_wing Desc="Auftriebsbeiwert bei bestem LoverD (Anteil Fluegel)" ToolLevel="1" Unit="-">0.56482909</C_L_opt_wing>
+            <C_L_opt_stab Desc="Auftriebsbeiwert bei bestem LoverD (Anteil HLW)" ToolLevel="1" Unit="-">-0.03082906473</C_L_opt_stab>
+            <C_LgroundRoll Desc="lift coefficient on ground for ground roll calculation" ToolLevel="1" Unit="-">0.4</C_LgroundRoll>
+        </LiftCoefficients>
+        <DragCoefficients Desc="Widerstandsbeiwerte (bei bestem L/D im Cruise, s.o.)">
+            <C_D_total Desc="Widerstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.03127999549</C_D_total>
+            <C_D_ind Desc="induzierter Widerstandsbeiwert" ToolLevel="1" Unit="-">0.01011147857</C_D_ind>
+            <C_D_visc Desc="Reibungswiderstandsbeiwerte" ToolLevel="1" Unit="-">
+                <C_D_visc_total Desc="Reibungswiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.01998021606</C_D_visc_total>
+                <C_D_visc_wing Desc="Reibungswiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.006065898162</C_D_visc_wing>
+                <C_D_visc_stab Desc="Reibungswiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0.001539217794</C_D_visc_stab>
+                <C_D_visc_fin Desc="Reibungswiderstandsbeiwert SLW" ToolLevel="1" Unit="-">0.001759127689</C_D_visc_fin>
+                <C_D_visc_fus Desc="Reibungswiderstandsbeiwert Rumpf" ToolLevel="1" Unit="-">0.006881721154</C_D_visc_fus>
+                <C_D_visc_nac Desc="Reibungswiderstandsbeiwert Nacelle" ToolLevel="1" Unit="-">0.001626766969</C_D_visc_nac>
+                <C_D_visc_misc Desc="Reibungswiderstandsbeiwert weitere" ToolLevel="1" Unit="-">0.002107484288</C_D_visc_misc>
+            </C_D_visc>
+            <C_D_wave Desc="Wellenwiderstandsbeiwerte" ToolLevel="1" Unit="-">
+                <C_D_wave_total Desc="Wellenwiderstandsbeiwert gesamt" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_total>
+                <C_D_wave_wing Desc="Wellenwiderstandsbeiwert Fluegel" ToolLevel="1" Unit="-">0.00118830087</C_D_wave_wing>
+                <C_D_wave_stab Desc="Wellenwiderstandsbeiwert HLW" ToolLevel="1" Unit="-">0</C_D_wave_stab>
+            </C_D_wave>
+            <EoW_DragFactor Desc="Drag factor for over-the-wing engines" ToolLevel="1" Unit="-">1</EoW_DragFactor>
+        </DragCoefficients>
+        <MomentCoefficients Desc="Momentenbeiwerte (getrimmt, bei bestem L/D im Cruise, s.o.)">
+            <C_M_total Desc="Momentenbeiwert bei optimum Cruise" ToolLevel="1" Unit="-">-0.001284519415</C_M_total>
+        </MomentCoefficients>
+        <Polar Desc="Flugzeugpolare">
+            <PolarFile Desc="Dateiname der Flugzeugpolare" ToolLevel="1" Unit="-">CSR_polar.xml</PolarFile>
+            <Configurations Desc="Anzahl der aerodynamischen Konfigurationen in der Polarendatei" ToolLevel="1">7</Configurations>
+            <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="1" ToolLevel="1" Type="Cruise">Clean</Configuration>
+            <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="2" ToolLevel="1" Type="Departure">TakeOff</Configuration>
+            <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="3" ToolLevel="1" Type="Departure">TakeOffLGRetracted</Configuration>
+            <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="4" ToolLevel="1" Type="Departure">Climb</Configuration>
+            <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="5" ToolLevel="1" Type="Approach">Approach</Configuration>
+            <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="6" ToolLevel="1" Type="Approach">ApproachLG</Configuration>
+            <Configuration Desc="Konfiguration im Polaren-File mit der ID gekennzeichnet. name kann abweichend definiert sein" ID="7" ToolLevel="1" Type="Approach">Landing</Configuration>
+        </Polar>
+        <ReferenceValues Desc="Aerodynamische Bezugsgroessen">
+            <b Desc="Total wing span" ToolLevel="1" Unit="m">34.10358666</b>
+            <MAC Desc="Mean aerodynamic chord" ToolLevel="1" Unit="m">4.331683874</MAC>
+            <S_ref Desc="Wing reference area" ToolLevel="1" Unit="m2">122.4268024</S_ref>
+        </ReferenceValues>
+        <MaxSpoilerFactor Desc="Faktor zur max. Widerstandserhoehung durch Spoiler" ToolLevel="1" Unit="-">2.5</MaxSpoilerFactor>
+    </Aerodynamics>
+    <StabilityAndControlCharacteristics Desc="Flugmechanik, Stabilitaet und Steuerbarkeit">
+        <Stabiliser>
+            <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">1.03545133</VolumeCoefficient>
+            <S_ref Desc="Stabiliser reference area" ToolLevel="1" Unit="m2">32.46074351</S_ref>
+        </Stabiliser>
+        <VerticalTail>
+            <VolumeCoefficient Desc="berechneter Volumenkoeffizient" Matched="1" ToolLevel="1" Unit="-">0.1018345125</VolumeCoefficient>
+            <S_ref Desc="Fin reference area" ToolLevel="1" Unit="m2">26.57458461</S_ref>
+        </VerticalTail>
+    </StabilityAndControlCharacteristics>
+    <Performance Desc="Flugleistungen">
+        <Range Desc="Reichweiten">
+            <Range_maxPayloadatMTOM Desc="Reichweite bei maximaler Nutzlast und Betankung bis zum MTOM-Limit" ToolLevel="2" Unit="km">3043.938845</Range_maxPayloadatMTOM>
+            <Range_maxFuelatMTOM Desc="Reichweite bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="km">11558.21333</Range_maxFuelatMTOM>
+            <Payload_maxFuelatMTOM Desc="Payload bei vollen Tanks und Nutzlast bis zum MTOM-Limit" ToolLevel="2" Unit="kg">3895.43595</Payload_maxFuelatMTOM>
+            <Range_maxFuelEmpty Desc="Ueberfuehrungsreichweite, leer mit vollen Tanks" ToolLevel="2" Unit="km">12572.68487</Range_maxFuelEmpty>
+        </Range>
+        <Speed Desc="Fluggeschwindigkeiten">
+            <M_initialCruise Desc="Cruisemachzahl" ToolLevel="3" Unit="-">0.78</M_initialCruise>
+            <M_maxOperating Desc="Max Operating Cruise Machzahl" ToolLevel="2" Unit="-">0.82</M_maxOperating>
+            <V_maxOperating Desc="Max Operating Speed (Maximale Staudruckgeschwindigkeit CAS/IAS)" ToolLevel="2" Unit="KCAS">350</V_maxOperating>
+            <M_Dive Desc="Diving Mach Number" ToolLevel="2" Unit="-">0.902</M_Dive>
+            <V_Dive Desc="Diving Speed" ToolLevel="2" Unit="KCAS">385</V_Dive>
+            <V_s1g Desc="1-g Stalling Speed" ToolLevel="2" Unit="KCAS">161.952013</V_s1g>
+        </Speed>
+        <Altitudes Desc="Flughoehen">
+            <h_initialCruise Desc="Reiseflughoehe" ToolLevel="3" Unit="m">10058.4</h_initialCruise>
+            <h_maxCertified Desc="maximal zugelassene Flughoehe (s. TLAR)" ToolLevel="3" Unit="m">11734.8</h_maxCertified>
+            <h_maxOperating Desc="Dienstgipfelhoehe (100 ft/min Steigkriterium)" ToolLevel="3" Unit="m">12010.7005</h_maxOperating>
+            <h_maxCeiling Desc="Maximale Flughoehe (50 ft/min Steigkriterium) bei MTOM" ToolLevel="3" Unit="m">12053.19642</h_maxCeiling>
+            <h_maxOEI Desc="Maximale Flughoehe (100 ft/min Steigkriterium) bei einem Triebwerksausfall und bei MTOM" ToolLevel="3" Unit="m">7730.61576</h_maxOEI>
+        </Altitudes>
+        <Climb Desc="Steigflug">
+            <TTC_Design Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">14.56137643</TTC_Design>
+            <Time_to_1500ft_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10>
+            <Time_to_ICA_ISA10 Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="min">15.53402313</Time_to_ICA_ISA10>
+            <Range_to_ICA_ISA10 Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="NM">89.09881839</Range_to_ICA_ISA10>
+            <Fuel_to_ICA_ISA10 Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10)" ToolLevel="3" Unit="kg">1577.91233</Fuel_to_ICA_ISA10>
+            <TTC_ISA Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA>
+            <Time_to_1500ft_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA>
+            <Time_to_ICA_ISA Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA>
+            <Range_to_ICA_ISA Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA>
+            <Fuel_to_ICA_ISA Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA>
+            <TTC_ISA10_optROC Desc="Benoetigte Zeit fuer Steigen von 1500ft bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">5.079260451</TTC_ISA10_optROC>
+            <Time_to_1500ft_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis 1500ft (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">0.9726466934</Time_to_1500ft_ISA10_optROC>
+            <Time_to_ICA_ISA10_optROC Desc="Benoetigte Zeit fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="min">6.051907144</Time_to_ICA_ISA10_optROC>
+            <Range_to_ICA_ISA10_optROC Desc="Benoetigte Range fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="NM">22.96381264</Range_to_ICA_ISA10_optROC>
+            <Fuel_to_ICA_ISA10_optROC Desc="Benoetigter Treibstoff fuer Steieigen von BR bis auf ICA (ISA+10, opt. ROC)" ToolLevel="3" Unit="kg">732.9613247</Fuel_to_ICA_ISA10_optROC>
+        </Climb>
+        <TakeOff Desc="Start Performance">
+            <TakeOffDistance_Normal Desc="Startstrecke - Normalstartstrecke bei MTOM und ISA+15" ToolLevel="2" Unit="m">1731.705965</TakeOffDistance_Normal>
+            <BFL Desc="Startstrecke - Balanced Fieldlength bei MTOM und ISA+15 " ToolLevel="2" Unit="m">1853.411621</BFL>
+            <TimeToScreenHeight Desc="Zeit bis zum erreichen von 35 ft" ToolLevel="2" Unit="s">34.72221827</TimeToScreenHeight>
+            <V_LOF Desc="Abhebegeschwindigkeit" ToolLevel="2" Unit="KCAS">136.8991062</V_LOF>
+            <V_1 Desc="Decision Speed bei fuer MTOM BLFL" ToolLevel="2" Unit="KCAS">135.3462489</V_1>
+            <V_2 Desc="Geschwindigkeit auf Screen height (35 ft)" ToolLevel="2" Unit="KCAS">136.8991062</V_2>
+            <V_FTO Desc="Geschwindigkeit am Ende des Final T-O Segment (1500 ft)" ToolLevel="2" Unit="KCAS">203.0413711</V_FTO>
+            <ScdSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.68313876</ScdSegmentClimbGradient>
+            <FinalSegmentClimbGradient Desc="Steigradient im zweiten Steigsegment TO" ToolLevel="2" Unit="%">2.683126144</FinalSegmentClimbGradient>
+        </TakeOff>
+        <Landing>
+            <LandingDistance Desc="Landestrecke" ToolLevel="2" Unit="m">1528.071526</LandingDistance>
+            <V_Approach Desc="Anfluggeschwindigkeit" ToolLevel="2" Unit="KCAS">129.2323788</V_Approach>
+        </Landing>
+        <MissionAnalysis Desc="Missionsanalyse">
+            <DesignMission Desc="Parameter der Design-Mission">
+                <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionDesign.xml</MissionFile>
+                <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">2</CruiseSteps>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">0.5008065466</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">330.0000005</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">18070.1076</Missionfuel>
+                <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">14883.27019</Tripfuel>
+                <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff>
+                <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg>
+                <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">5.947085161</Blocktime>
+                <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">5.713751827</Flighttime>
+                <Range Desc="Range" ToolLevel="3" Unit="NM">2500.55303</Range>
+                <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">76962.57512</TOM>
+                <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">17000</Payload>
+                <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
+                <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">3392</CargoMass>
+                <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
+                <Offtakes>
+                    <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
+                        <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">73.40008433</ShaftPowerTotal>
+                        <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal>
+                    </AverageCruiseOfftakes>
+                </Offtakes>
+                <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
+                    <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.5148367758</CL_avg>
+                    <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4915188994</CL_min>
+                    <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.5675400636</CL_max>
+                </LiftCoefficientsCruise>
+                <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
+                    <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">75060.13292</Mass_TOC>
+                    <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">62441.91279</Mass_TOD>
+                </MassesCruise>
+            </DesignMission>
+            <StudyMission Desc="Parameter der Study-Mission">
+                <MissionFile Desc="Dateiname der Missionsdatei" ToolLevel="1" Unit="-">missionStudy.xml</MissionFile>
+                <CruiseSteps Desc="Anzahl der Hoehenschritte im Reiseflug-Missionsprofil" ToolLevel="3">1</CruiseSteps>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="1">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="3" Unit="-">1</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="3" Unit="FL">350.0000005</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="2">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="3">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="4">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="5">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="6">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="7">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="8">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="9">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="10">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="11">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="12">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="13">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="14">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <CruiseStep Desc="Beschreibung eines Cruise-Steps" ID="15">
+                    <RelStepLength Desc="Rel. Laenge des Cruise-Steps bezogen auf Reiseflug-Strecke" ToolLevel="1" Unit="-">0</RelStepLength>
+                    <FlightLevel Desc="Flight Level des Cruise-Steps" ToolLevel="1" Unit="FL">0</FlightLevel>
+                </CruiseStep>
+                <Missionfuel Desc="Getankter Kraftstoff (Tripfuel + Reserve Fuel + TaxifuelTakeoff)" ToolLevel="3" Unit="kg">5967.411758</Missionfuel>
+                <Tripfuel Desc="Tripfuel (Fuel burned from takeoff to landing)" ToolLevel="3" Unit="kg">3241.768614</Tripfuel>
+                <TaxifuelTakeoff Desc="Taxifuel vor dem Start" ToolLevel="3" Unit="kg">90.32770904</TaxifuelTakeoff>
+                <TaxifuelLdg Desc="Taxifuel nach der Landung" ToolLevel="3" Unit="kg">50.18206058</TaxifuelLdg>
+                <Blocktime Desc="Blocktime" ToolLevel="3" Unit="h">1.50538405</Blocktime>
+                <Flighttime Desc="Flugzeit ohne taxi" ToolLevel="3" Unit="h">1.272050716</Flighttime>
+                <Range Desc="Range" ToolLevel="3" Unit="NM">500.546566</Range>
+                <TOM Desc="geflogenes Take Off Mass" ToolLevel="3" Unit="kg">61467.87928</TOM>
+                <Payload Desc="geflogene Payload" ToolLevel="3" Unit="kg">13608</Payload>
+                <NumberOfPAX Desc="Anzahl Passagiere" ToolLevel="3" Unit="-">150</NumberOfPAX>
+                <CargoMass Desc="Frachtmasse" ToolLevel="3" Unit="kg">0</CargoMass>
+                <TakeOffEngineDerate Desc="Engine Derate (AMTC,eng); reduced takeoff-thrust" ToolLevel="3" Unit="-">1</TakeOffEngineDerate>
+                <Offtakes>
+                    <AverageCruiseOfftakes Desc="Durschnittliche Entnahmen fuer Cruise-Modes Cruise und ChangeFL">
+                        <ShaftPowerTotal Desc="Gesamte Wellenleistungsentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kW">72.97412478</ShaftPowerTotal>
+                        <BleedAirTotal Desc="Gesamte Zapfluftentnahme durch alle Systeme (Sinks)" ToolLevel="1" Unit="kg/s">0.9793842105</BleedAirTotal>
+                    </AverageCruiseOfftakes>
+                </Offtakes>
+                <LiftCoefficientsCruise Desc="Erflogene Auftriebsbeiwerte im Reiseflug">
+                    <CL_avg Desc="Arithm. Mittelwert ueber gesamten Reiseflug" ToolLevel="3" Unit="-">0.4681348875</CL_avg>
+                    <CL_min Desc="Min. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4621586298</CL_min>
+                    <CL_max Desc="Max. Wert fuer gesamten Reiseflug" ToolLevel="3" Unit="-">0.4991350396</CL_max>
+                </LiftCoefficientsCruise>
+                <MassesCruise Desc="Gesamtflugzeugmassen waehrend des Reiseflugs">
+                    <Mass_TOC Desc="Gesamtflugzeugmasse am Top-of-Climb-Punkt (ICA)" ToolLevel="3" Unit="kg">60071.12337</Mass_TOC>
+                    <Mass_TOD Desc="Gesamtflugzeugmasse am Top-of-Descent-Punkt" ToolLevel="3" Unit="kg">58584.28057</Mass_TOD>
+                </MassesCruise>
+            </StudyMission>
+        </MissionAnalysis>
+        <RequirementsChecks>
+            <MissionFile Desc="Dateiname der Missionsdatei" OfftakesWritten="1" ToolLevel="1" Unit="-">missionReq.xml</MissionFile>
+            <TLARs>
+                <TOFL_Design Checked="1" ToolLevel="2">1</TOFL_Design>
+                <LDN_Design Checked="1" ToolLevel="2">1</LDN_Design>
+                <V_ApproachSpeed_Design Checked="1" ToolLevel="2">1</V_ApproachSpeed_Design>
+                <h_initialCruise_Design Checked="1" ToolLevel="3">1</h_initialCruise_Design>
+                <h_maxOperating Checked="1" ToolLevel="3">1</h_maxOperating>
+                <h_maxOEI Checked="1" ToolLevel="3">1</h_maxOEI>
+                <M_initialCruise_Design Checked="1" ToolLevel="3">1</M_initialCruise_Design>
+                <TTC_Design Checked="1" ToolLevel="3">1</TTC_Design>
+            </TLARs>
+            <Certification>
+                <climbGradientSecondTOSegment Checked="1" ToolLevel="2">1</climbGradientSecondTOSegment>
+                <climbGradientFinalTOSegment Checked="1" ToolLevel="2">1</climbGradientFinalTOSegment>
+                <climbGradientApproachOEI Checked="1" ToolLevel="2">1</climbGradientApproachOEI>
+                <climbGradientApproachAEO Checked="1" ToolLevel="2">1</climbGradientApproachAEO>
+            </Certification>
+        </RequirementsChecks>
+    </Performance>
+    <MonetaryValues Desc="Kosten und Preise">
+        <MonetaryScenario>
+            <AirframeEngineeringHours Desc="Anzahl der Arbeitsstunden in der FZ-Entwicklung" ToolLevel="1" Unit="h">12079799</AirframeEngineeringHours>
+            <ProductionVolume Desc="Anzahl produzierter Flugzeuge je Programm" ToolLevel="1">1500</ProductionVolume>
+        </MonetaryScenario>
+        <Earnings Desc="Herstellergewinn pro verkauftem Flugzeug" ToolLevel="1" Unit="$">28158406</Earnings>
+        <NPV Desc="Net Present Value (Kapitalwert) fuer Flugzeugprogramm bei Verkauf des gesamten ProductionVolume" ToolLevel="1" Unit="Mio.$">33855.557</NPV>
+        <Prices Desc="Preise">
+            <PriceAirplane Desc="airplane price (for the whole plane); for the insurance and for the Simple_deprecition in DOC-Tool" ToolLevel="1" Unit="$">71228241.8</PriceAirplane>
+            <DiscountRate Desc="discount rate on airplane lst price granted airlines" ToolLevel="1" Unit="-">0.07</DiscountRate>
+        </Prices>
+        <LCC Desc="Life Cycle Costs">
+            <NonRecurringCosts Desc="Non-Recurring Costs fuer gesamtes Flugzeugprogramm">
+                <NRCTotal Desc="Non Recurring Costs" ToolLevel="1" Unit="$">3475793421</NRCTotal>
+                <NRCComponents>
+                    <AirframeEngAndDesign Desc="Costs for Airframe Engineering and Design" ToolLevel="1" Unit="$">1359777460</AirframeEngAndDesign>
+                    <DevSupportAndTesting Desc="Costs for Development Support and Testing" ToolLevel="1" Unit="$">345988343</DevSupportAndTesting>
+                    <FlightTestAC>
+                        <FlightTestACTotal Desc="Costs for Flight Test Aircraft" ToolLevel="1" Unit="$">1636269510</FlightTestACTotal>
+                        <FlightTestACComponents>
+                            <EngineAndAvionics Desc="Costs for Engines and Avionics" ToolLevel="1" Unit="$">117031730</EngineAndAvionics>
+                            <LaborManufacturing Desc="Costs for Manufacturing Labor" ToolLevel="1" Unit="$">622590665</LaborManufacturing>
+                            <MaterialManufacturing Desc="Costs for Manufacturing Material" ToolLevel="1" Unit="$">188900611</MaterialManufacturing>
+                            <Tooling Desc="Costs for Tooling" ToolLevel="1" Unit="$">624941946</Tooling>
+                            <QualityControl Desc="Costs for Quality Control" ToolLevel="1" Unit="$">82804558</QualityControl>
+                        </FlightTestACComponents>
+                    </FlightTestAC>
+                    <FlightTestOp Desc="Costs for Flight Test Operations" ToolLevel="1" Unit="$">133758109</FlightTestOp>
+                    <Facilities Desc="Costs for Test and Simulation Facilities" ToolLevel="1" Unit="$">0</Facilities>
+                </NRCComponents>
+            </NonRecurringCosts>
+            <RecurringCosts Desc="Recurring Costs">
+                <RCTotal Desc="Recurring Costs" ToolLevel="1" Unit="$">35766663</RCTotal>
+                <RCComponents>
+                    <Wing Desc="Costs for Wing" ToolLevel="1" Unit="$">2408072</Wing>
+                    <Fuselage Desc="Costs for Fuselage" ToolLevel="1" Unit="$">2957731</Fuselage>
+                    <Empennage Desc="Costs for Empennage" ToolLevel="1" Unit="$">584113</Empennage>
+                    <LandingGear Desc="Costs for Landing Gear" ToolLevel="1" Unit="$">639568</LandingGear>
+                    <Pylons Desc="Costs for Pylons" ToolLevel="1" Unit="$">879551</Pylons>
+                    <PowerUnit Desc="Costs for all installed engines with systems without pylons">
+                        <PowerUnitTotal Desc="Costs for PowerUnit" ToolLevel="1" Unit="$">13337566</PowerUnitTotal>
+                        <PowerUnitComponents>
+                            <EquippedEngines Desc="Costs for Engines Dry and Other Systems" ToolLevel="1" Unit="$">11357394</EquippedEngines>
+                            <Nacelles Desc="Costs for Nacelles" ToolLevel="1" Unit="$">1791842</Nacelles>
+                            <BleedAirSystem Desc="Costs for BleedAirSystem (Airbus Chapter 21, ATA36)" ToolLevel="1" Unit="$">107416</BleedAirSystem>
+                            <FuelSystem Desc="Costs for Fuel System (Airbus Chapter 23, ATA28)" ToolLevel="1" Unit="$">80914</FuelSystem>
+                        </PowerUnitComponents>
+                    </PowerUnit>
+                    <Systems>
+                        <SystemsTotal Desc="Costs for Systems" ToolLevel="1" Unit="$">7436254</SystemsTotal>
+                        <SystemsComponents>
+                            <APU Desc="Costs for APU (Airbus Chapter 30, ATA49)" ToolLevel="1" Unit="$">273442</APU>
+                            <HydraulicSystem Desc="Costs for Hydraulic System (Airbus Chapter 31 + 32,ATA29)" ToolLevel="1" Unit="$">220982</HydraulicSystem>
+                            <AirConditioning Desc="Costs for Air Conditioning (Airbus Chapter 33, ATA21)" ToolLevel="1" Unit="$">694499</AirConditioning>
+                            <DeIcing Desc="Costs for De-Icing (Airbus Chapter 34, ATA30)" ToolLevel="1" Unit="$">40295</DeIcing>
+                            <FireProtection Desc="Costs for Fire Protection (Airbus Chapter 35, ATA26)" ToolLevel="1" Unit="$">39314</FireProtection>
+                            <FlightControls Desc="Costs for Flight Controls (Airbus Chapter 36, ATA27)" ToolLevel="1" Unit="$">598096</FlightControls>
+                            <Instruments Desc="Costs for Instruments (Airbus Chapter 37, ATA31)" ToolLevel="1" Unit="$">343899</Instruments>
+                            <AutomaticFlightSystem Desc="Costs for Automatic Flight System (Airbus Chapter 38, ATA22)" ToolLevel="1" Unit="$">558835</AutomaticFlightSystem>
+                            <Navigation Desc="Costs for Navigation (Airbus Chapter 39, ATA34)" ToolLevel="1" Unit="$">2278329</Navigation>
+                            <Communication Desc="Costs for Communication (Airbus Chapter 40, ATA23)" ToolLevel="1" Unit="$">1117671</Communication>
+                            <ElectricalSystem Desc="Costs for Air Conditioning (Airbus Chapter 41+42, ATA24)" ToolLevel="1" Unit="$">1270893</ElectricalSystem>
+                        </SystemsComponents>
+                    </Systems>
+                    <Furnishings>
+                        <FurnishingsTotal Desc="Costs for Furnishings" ToolLevel="1" Unit="$">1442699</FurnishingsTotal>
+                        <FurnishingsComponents>
+                            <Furnishing Desc="Costs for Furnishings (Airbus Chapter 50, ATA25)" ToolLevel="1" Unit="$">1048900</Furnishing>
+                            <FixedEmergencyOxygen Desc="Costs for Fixed Emergency Oxygen (Airbus Chapter 51, ATA35)" ToolLevel="1" Unit="$">41911</FixedEmergencyOxygen>
+                            <Lighting Desc="Costs for Lighting (Airbus Chapter 52, ATA33)" ToolLevel="1" Unit="$">228444</Lighting>
+                            <WaterInstallation Desc="Costs for Water Installation (Airbus Chapter 53, ATA38)" ToolLevel="1" Unit="$">123443</WaterInstallation>
+                        </FurnishingsComponents>
+                    </Furnishings>
+                    <OperatorsItems Desc="Costs for OperatorItems (Airbus Chapter 60+61)" ToolLevel="1" Unit="$">1415894</OperatorsItems>
+                    <FinalAssembly Desc="Costs for FinalAssembly" ToolLevel="1" Unit="$">4665217</FinalAssembly>
+                </RCComponents>
+            </RecurringCosts>
+            <OperatingCosts>
+                <OperatingScenario Desc="Umrechnungsfaktor fuer verschiedene DOC-Einheiten, zusaetzlich aus A/C-XML: Nseats=PassengersTotal">
+                    <FlightsPerYear Desc="Flights per year / take-offs annually; aus operating_company.xml" ToolLevel="1" Unit="">2230</FlightsPerYear>
+                    <SeatLoadFactor Desc="utilisation factor for the payload; aus operating_company.xml" ToolLevel="1" Unit="">1</SeatLoadFactor>
+                </OperatingScenario>
+                <DirectOperatingCosts>
+                    <DOC_total Desc="Summe aller DOCComponents (s.u)">
+                        <DOC_year Desc="DOC pro Jahr" ToolLevel="1" Unit="$/year">20437514.98</DOC_year>
+                        <DOC_FH Desc="DOC pro Flugstunde = DOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7204.76</DOC_FH>
+                        <DOC_flight Desc="DOC pro Flug = DOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9164.81</DOC_flight>
+                        <DOC_km Desc="DOC pro km = DOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">9.9</DOC_km>
+                        <DOC_100ASK Desc="DOC pro 100 Available Seat Kilometer = DOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.6</DOC_100ASK>
+                    </DOC_total>
+                    <COC_total Desc="Summe aller DOCComponents ausser Depreciation und Insurance">
+                        <COC_year Desc="COC pro Jahr" ToolLevel="1" Unit="$/year">17054173.5</COC_year>
+                        <COC_FH Desc="COC pro Flugstunde = COC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">6012.05</COC_FH>
+                        <COC_flight Desc="COC pro Flug = COC_year/(Nta)" ToolLevel="1" Unit="$/flight">7647.62</COC_flight>
+                        <COC_km Desc="COC pro km = COC_year/(Nta*R)" ToolLevel="1" Unit="$/km">8.26</COC_km>
+                        <COC_100ASK Desc="COC pro 100 Available Seat Kilometer = COC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">5.50770807</COC_100ASK>
+                    </COC_total>
+                    <DOCComponents Desc="DOC-Anteile in 100ASK">
+                        <Charge Desc="Gebuehren pro 100ASK">
+                            <ChargeTotal Desc="total charges" ToolLevel="1" Unit="$/100ASK">1.83</ChargeTotal>
+                            <ChargesComponents>
+                                <NavigationCharge Desc="navigational charges" ToolLevel="1" Unit="$/100ASK">0.73</NavigationCharge>
+                                <LandingCharge Desc="landing charges" ToolLevel="1" Unit="$/100ASK">0.33</LandingCharge>
+                                <LandingChargeComponents>
+                                    <NoiseCharge Desc="noise charges" ToolLevel="1" Unit="$/100ASK">0</NoiseCharge>
+                                    <NOxCharge Desc="NOx charges" ToolLevel="1" Unit="$/100ASK">0</NOxCharge>
+                                    <ChargeWithoutEmission Desc="landing charges without emissions (noise + NOx)" ToolLevel="1" Unit="$/100ASK">0.33</ChargeWithoutEmission>
+                                </LandingChargeComponents>
+                                <GroundCharge Desc="ground charges" ToolLevel="1" Unit="$/100ASK">0.77</GroundCharge>
+                            </ChargesComponents>
+                        </Charge>
+                        <Depreciation Desc="Abschreibungskosten" ToolLevel="1" Unit="$/100ASK">0.98</Depreciation>
+                        <Insurance Desc="Versicherungskosten" ToolLevel="1" Unit="$/100ASK">0.11</Insurance>
+                        <Maintenance Desc="Wartungskosten">
+                            <MaintenanceTotal Desc="Wartungskosten gesamt" ToolLevel="1" Unit="$/100ASK">0.75</MaintenanceTotal>
+                            <MaintenanceComponents>
+                                <Airframe Desc="Wartungskosten Airframe">
+                                    <AirframeTotal Desc="Wartungskosten Airframe gesamt" ToolLevel="1" Unit="$/100ASK">0.3</AirframeTotal>
+                                    <CostComponents>
+                                        <LabourCosts Desc="Arbeitskosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.243</LabourCosts>
+                                        <MaterialCosts Desc="Materialkosten Wartung Airframe" ToolLevel="1" Unit="$/100ASK">0.061</MaterialCosts>
+                                    </CostComponents>
+                                    <AirframeComponents Desc="Kostenwert fuer das ATA Kapitel">
+                                        <ATA21 Desc="Environmental Control System">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0134</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0107</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0027</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA21>
+                                        <ATA22 Desc="Autoflight">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0127</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0102</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA22>
+                                        <ATA23 Desc="Communications">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0123</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0098</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0025</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA23>
+                                        <ATA24 Desc="Electrical System">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0211</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0169</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0042</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA24>
+                                        <ATA25 Desc="Furnishing">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0409</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0327</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0082</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA25>
+                                        <ATA26 Desc="Fire Protection">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0043</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0035</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0009</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA26>
+                                        <ATA27 Desc="Flight Control System">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.025</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.02</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.005</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA27>
+                                        <ATA28 Desc="Fuel System">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0022</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA28>
+                                        <ATA29 Desc="Hydraulic System">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0131</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0105</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0026</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA29>
+                                        <ATA30 Desc="Ice and Rain Protection">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA30>
+                                        <ATA31 Desc="Instrumentation">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0013</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0003</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA31>
+                                        <ATA32 Desc="Landing Gear">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0559</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0447</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0112</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA32>
+                                        <ATA33 Desc="Lights">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0051</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0041</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA33>
+                                        <ATA34 Desc="Navigation">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0142</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0113</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0028</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA34>
+                                        <ATA35 Desc="Oxygen">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.003</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0006</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA35>
+                                        <ATA36 Desc="Pneumatic">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0036</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0029</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0007</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA36>
+                                        <ATA38 Desc="Water and Waste">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0024</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0019</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0005</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA38>
+                                        <ATA49 Desc="APU">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0104</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0083</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0021</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA49>
+                                        <ATA51 Desc="Structure">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.004</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0032</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0008</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA51>
+                                        <ATA52 Desc="Doors">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0054</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0044</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA52>
+                                        <ATA53 Desc="Fuselage">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0057</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA53>
+                                        <ATA54 Desc="Nacelles">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0012</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.001</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0002</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA54>
+                                        <ATA55 Desc="Stabilizers">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0018</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0015</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0004</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA55>
+                                        <ATA56 Desc="Windows">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0081</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0065</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0016</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA56>
+                                        <ATA57 Desc="Wings">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0056</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0045</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0011</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA57>
+                                        <ATA99 Desc="Routinearbeiten, hauptsaechlich Inspektion">
+                                            <TotalCosts Desc="Total Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0294</TotalCosts>
+                                            <CostComponents>
+                                                <LabourCosts Desc="Labour Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0235</LabourCosts>
+                                                <MaterialCosts Desc="Material Costs of the Component" ToolLevel="1" Unit="$/100ASK">0.0059</MaterialCosts>
+                                            </CostComponents>
+                                        </ATA99>
+                                    </AirframeComponents>
+                                </Airframe>
+                                <Engine Desc="Wartungskosten Triebwerk" ToolLevel="1" Unit="$/100ASK">0.45</Engine>
+                            </MaintenanceComponents>
+                        </Maintenance>
+                        <Fuel Desc="Spritkosten" ToolLevel="1" Unit="$/100ASK">2.44</Fuel>
+                        <Crew Desc="Crew Kosten">
+                            <CrewTotal Desc="Crew Kosten gesamt" ToolLevel="1" Unit="$/100ASK">0.49</CrewTotal>
+                            <CrewComponents>
+                                <FlightCrew Desc="Flight Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.12</FlightCrew>
+                                <CabinCrew Desc="Cabin Crew Kosten" ToolLevel="1" Unit="$/100ASK">0.36</CabinCrew>
+                            </CrewComponents>
+                        </Crew>
+                        <Delay Desc="Verspaetungskosten" ToolLevel="1" Unit="$/100ASK">0</Delay>
+                    </DOCComponents>
+                </DirectOperatingCosts>
+                <IndirectOperatingCosts>
+                    <IOC_total Desc="Summe aller IOCComponents (s.u)">
+                        <IOC_year Desc="IOC pro Jahr" ToolLevel="1" Unit="$/year">20699680.51</IOC_year>
+                        <IOC_FH Desc="IOC pro Flugstunde = IOC_year/(Nta*Tflight)" ToolLevel="1" Unit="$/FH">7297.17</IOC_FH>
+                        <IOC_flight Desc="IOC pro Flug = IOC_year/(Nta)" ToolLevel="1" Unit="$/flight">9282.37</IOC_flight>
+                        <IOC_km Desc="IOC pro km = IOC_year/(Nta*R)" ToolLevel="1" Unit="$/km">10.02</IOC_km>
+                        <IOC_100ASK Desc="IOC pro 100 Available Seat Kilometer = IOC_year/(Nta*R*Nseats)" ToolLevel="1" Unit="$/100ASK">6.68</IOC_100ASK>
+                    </IOC_total>
+                </IndirectOperatingCosts>
+            </OperatingCosts>
+            <EndOfLifeCosts>
+                <EOLCTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="$">48616</EOLCTotal>
+                <EOLCTotalComponents>
+                    <TransportToEoLSite Desc="Kosten fuer Transport zur Abwrack-Location" ToolLevel="1" Unit="$">9140</TransportToEoLSite>
+                    <DisassemblyAndDismantling Desc="Kosten fuer Dissassembly and Dismantling" ToolLevel="1" Unit="$">124837</DisassemblyAndDismantling>
+                    <Recycling Desc="Materialrecycling, bei negativem Wert Benefit durch Materialverkauf" ToolLevel="1" Unit="$">-86485</Recycling>
+                    <Incineration Desc="Kosten fuer Verbrennung (inkl. shredding, mixing, incineration, and landfill of ash) " ToolLevel="1" Unit="$">297</Incineration>
+                    <Landfill Desc="Kosten fuer Landfill" ToolLevel="1" Unit="$">827</Landfill>
+                </EOLCTotalComponents>
+            </EndOfLifeCosts>
+        </LCC>
+    </MonetaryValues>
+    <EcologicalValues Desc="Oekologische Bewertung">
+        <Noise Desc="Akustische Kenngroessen und Laermbewertungsmasse">
+            <NoisePathFiles>
+                <Departure Desc="Dateiname des Departure Path" ToolLevel="1">0</Departure>
+                <Approach Desc="Dateiname des Approach Path" ToolLevel="1">0</Approach>
+            </NoisePathFiles>
+            <NoiseCertificationLevels>
+                <LateralPoint>
+                    <LateralFullPower Desc="EPNL Sideline Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</LateralFullPower>
+                    <SPL Desc="dBA at lateral point" ToolLevel="1" Unit="dBA">0</SPL>
+                    <Loudness Desc="Loudness at lateral point" ToolLevel="1" Unit="Sone">0</Loudness>
+                    <Tonality Desc="Tonality at lateral point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+                    <Sharpness Desc="Sharpness at lateral point" ToolLevel="1" Unit="Acum">0</Sharpness>
+                    <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at lateral point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+                </LateralPoint>
+                <FlyoverPoint>
+                    <Flyover Desc="EPNL Flyover Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Flyover>
+                    <SPL Desc="dBA at flyover point" ToolLevel="1" Unit="dBA">0</SPL>
+                    <Loudness Desc="Loudness at flyover point" ToolLevel="1" Unit="Sone">0</Loudness>
+                    <Tonality Desc="Tonality at flyover point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+                    <Sharpness Desc="Sharpness at flyover point" ToolLevel="1" Unit="Acum">0</Sharpness>
+                    <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at flyover point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+                </FlyoverPoint>
+                <ApproachPoint>
+                    <Approach Desc="EPNL Approach Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</Approach>
+                    <SPL Desc="dBA at approach point" ToolLevel="1" Unit="dBA">0</SPL>
+                    <Loudness Desc="Loudness at approach point" ToolLevel="1" Unit="Sone">0</Loudness>
+                    <Tonality Desc="Tonality at approach point" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+                    <Sharpness Desc="Sharpness at approach point" ToolLevel="1" Unit="Acum">0</Sharpness>
+                    <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at approach point" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+                </ApproachPoint>
+                <CumulativeValues>
+                    <EPNdB Desc="EPNL Cumulative Zertifizierungspegel, ICAO Annex 16/3 und 16/4 Zertifizierungslaermpegel" ToolLevel="1" Unit="EPNdB">0</EPNdB>
+                    <SPL Desc="Cumulative dBA at the three points" ToolLevel="1" Unit="dBA">0</SPL>
+                    <Loudness Desc="Cumulative Loudness at the three points" ToolLevel="1" Unit="Sone">0</Loudness>
+                    <Tonality Desc="Tonality at the three points" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+                    <Sharpness Desc="Sharpness at the three points" ToolLevel="1" Unit="Acum">0</Sharpness>
+                    <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance at the three points" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+                </CumulativeValues>
+            </NoiseCertificationLevels>
+            <CommunityNoiseLevels>
+                <TakeOff>
+                    <SPL Desc="Sound Pressure Level 10km from brake release" ToolLevel="1" Unit="dBA">0</SPL>
+                    <SPLarea>
+                        <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
+                        <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
+                    </SPLarea>
+                    <PNLarea>
+                        <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
+                        <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
+                    </PNLarea>
+                    <PNLTarea>
+                        <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
+                        <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
+                    </PNLTarea>
+                    <EPNLarea>
+                        <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
+                        <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
+                    </EPNLarea>
+                    <LoudnessArea>
+                        <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
+                        <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Phon" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
+                    </LoudnessArea>
+                    <TonalityArea>
+                        <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
+                        <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.15 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
+                        <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
+                        <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.35 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
+                    </TonalityArea>
+                    <SharpnessArea>
+                        <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
+                        <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
+                    </SharpnessArea>
+                    <PsychoacousticAnnoyanceArea>
+                        <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
+                        <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
+                    </PsychoacousticAnnoyanceArea>
+                    <SELarea Desc="Sound Exposure Level area">
+                        <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
+                        <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
+                        <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
+                        <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
+                    </SELarea>
+                </TakeOff>
+                <Approach>
+                    <SPL Desc="Sound Pressure Level 15km from touchdown" ToolLevel="1" Unit="dBA">0</SPL>
+                    <SPLarea>
+                        <dBAthreshold1 Desc="Area of SPL higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold1>
+                        <dBAthreshold2 Desc="Area of SPL higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBAthreshold2>
+                    </SPLarea>
+                    <PNLarea>
+                        <PNLthreshold1 Desc="Area of PNL higher or equal than 65 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold1>
+                        <PNLthreshold2 Desc="Area of PNL higher or equal than 85 PNLdB" ToolLevel="1" Unit="km2">0</PNLthreshold2>
+                    </PNLarea>
+                    <PNLTarea>
+                        <PNLTthreshold1 Desc="Area of PNLT higher or equal than 65 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold1>
+                        <PNLTthreshold2 Desc="Area of PNLT higher or equal than 85 PNTdB" ToolLevel="1" Unit="km2">0</PNLTthreshold2>
+                    </PNLTarea>
+                    <EPNLarea>
+                        <EPNLthreshold1 Desc="Area of EPNL higher or equal than 65 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold1>
+                        <EPNLthreshold2 Desc="Area of EPNL higher or equal than 85 EPNdB" ToolLevel="1" Unit="km2">0</EPNLthreshold2>
+                    </EPNLarea>
+                    <LoudnessArea>
+                        <LoudnessThreshold1 Desc="Area of Zwickers loudness higher or equal than 65 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold1>
+                        <LoudnessThreshold2 Desc="Area of Zwickers loudness higher or equal than 85 Sone" ToolLevel="1" Unit="km2">0</LoudnessThreshold2>
+                    </LoudnessArea>
+                    <TonalityArea>
+                        <TonalityThreshold1 Desc="Area of tonality higher or equal than 0.075 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold1>
+                        <TonalityThreshold2 Desc="Area of tonality higher or equal than 0.10 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold2>
+                        <TonalityThreshold3 Desc="Area of tonality higher or equal than 0.20 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold3>
+                        <TonalityThreshold4 Desc="Area of tonality higher or equal than 0.25 tu" ToolLevel="1" Unit="km2">0</TonalityThreshold4>
+                    </TonalityArea>
+                    <SharpnessArea>
+                        <SharpnessThreshold1 Desc="Area of sharpness higher or equal than 0.75 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold1>
+                        <SharpnessThreshold2 Desc="Area of sharpness higher or equal than 1.0 acum" ToolLevel="1" Unit="km2">0</SharpnessThreshold2>
+                    </SharpnessArea>
+                    <PsychoacousticAnnoyanceArea>
+                        <PAthreshold1 Desc="Area of PA higher or equal than 10" ToolLevel="1" Unit="km2">0</PAthreshold1>
+                        <PAthreshold2 Desc="Area of PA higher or equal than 20" ToolLevel="1" Unit="km2">0</PAthreshold2>
+                    </PsychoacousticAnnoyanceArea>
+                    <SELarea Desc="Sound Exposure Level area">
+                        <dBA85 Desc="Area of Sound Exposure Level higher or equal than 85 dBA" ToolLevel="1" Unit="km2">0</dBA85>
+                        <dBA75 Desc="Area of Sound Exposure Level higher or equal than 75 dBA" ToolLevel="1" Unit="km2">0</dBA75>
+                        <dBA65 Desc="Area of Sound Exposure Level higher or equal than 65 dBA" ToolLevel="1" Unit="km2">0</dBA65>
+                        <dBA55 Desc="Area of Sound Exposure Level higher or equal than 55 dBA" ToolLevel="1" Unit="km2">0</dBA55>
+                    </SELarea>
+                </Approach>
+                <CumulativeValues>
+                    <EPNdB Desc="85 EPNdB area sum for takeoff and approach" ToolLevel="1" Unit="EPNdB">0</EPNdB>
+                    <SPL Desc="75 dBA area sum for takeoff and approach" ToolLevel="1" Unit="dBA">0</SPL>
+                    <Loudness Desc="85 Phon loudness area sum for takeoff and approach" ToolLevel="1" Unit="Sone">0</Loudness>
+                    <Tonality Desc="Tonality area sum for takeoff and approach - 0.1 t.u. for short-range and 0.2 t.u. for long-range AC" ToolLevel="1" Unit="tonality units t.u.">0</Tonality>
+                    <Sharpness Desc="1.0 Acum sharpness area sum for takeoff and approach" ToolLevel="1" Unit="Acum">0</Sharpness>
+                    <PsychoacousticAnnoyance Desc="Psychoacoustic Annoyance of 10 area sum for takeoff and approach" ToolLevel="1" Unit="-">0</PsychoacousticAnnoyance>
+                </CumulativeValues>
+            </CommunityNoiseLevels>
+        </Noise>
+        <Emissions>
+            <Development Desc="Analyse der Entwicklungsphase fuer gesamtes Flugzeugprogramm">
+                <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">11763648.53</CO2>
+                <H2O Desc="Wasser" ToolLevel="1" Unit="kg">40697548.71</H2O>
+                <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">22681.579</NOx>
+                <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">506.978</CO>
+                <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">10059.553</SO2>
+                <CH4 Desc="Methan" ToolLevel="1" Unit="kg">16890.095</CH4>
+                <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">176.255</PM10>
+                <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">982.444</N2O>
+                <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0.019</PFC>
+                <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">1432.078</NMVOC>
+                <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-4663.364</HC>
+            </Development>
+            <Production>
+                <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">618228.677</CO2>
+                <H2O Desc="Wasser" ToolLevel="1" Unit="kg">5361791.97</H2O>
+                <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">1320.026</NOx>
+                <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">1715.593</CO>
+                <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">2280.541</SO2>
+                <CH4 Desc="Methan" ToolLevel="1" Unit="kg">1327.591</CH4>
+                <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">5.711</PM10>
+                <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
+                <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
+                <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
+                <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-5.298</HC>
+            </Production>
+            <Operations>
+                <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">649479288.1</CO2>
+                <H2O Desc="Wasser" ToolLevel="1" Unit="kg">269362047.2</H2O>
+                <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">821056.648</NOx>
+                <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">279870.45</CO>
+                <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">533623.487</SO2>
+                <CH4 Desc="Methan" ToolLevel="1" Unit="kg">749253.374</CH4>
+                <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">10631.577</PM10>
+                <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
+                <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
+                <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
+                <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-247022.508</HC>
+                <OperationComponents>
+                    <ICAO_LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle gemaess ICAO Engine Emission Database und Standardzeiten fuer eine (!) StudyMission">
+                        <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">2844.948</CO2>
+                        <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">1084.134</H2O>
+                        <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.759</SO2>
+                        <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">99.106</HC>
+                        <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">5.747</CO>
+                        <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">11.071</NOx>
+                        <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.023</PM10>
+                    </ICAO_LTO>
+                    <Mission Desc="Environmental analysis of one study mission">
+                        <LTOTimes Desc="Times of LTO phases (all phases under 3000 ft)">
+                            <Total Desc="Taxi, Take-off, Climb Out and Approach time (LTO)" ToolLevel="1" Unit="min">19.622</Total>
+                            <TaxiTime Desc="Time for taxi (ICAO: 26 min)" ToolLevel="1" Unit="min">14</TaxiTime>
+                            <TakeOffTime Desc="Time for take-off (until 35ft) (ICAO: 0.7 min)" ToolLevel="1" Unit="min">0.311</TakeOffTime>
+                            <ClimbOutTime Desc="Time for climb out (35 ft to 3000ft)(ICAO: 2.2 min)" ToolLevel="1" Unit="min">0.933</ClimbOutTime>
+                            <ApproachTime Desc="Time for approach (from 3000 ft to stop)(ICAO: 4 min)" ToolLevel="1" Unit="min">4.377</ApproachTime>
+                        </LTOTimes>
+                        <LTO Desc="Triebwerksemissionen bestimmt nach dem LTO-Cycle mit Missionsanalyse fuer eine (!) StudyMission">
+                            <CO2 Desc="CO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">1500.242</CO2>
+                            <H2O Desc="H2O emitted during the LTO cycle" ToolLevel="1" Unit="kg">571.702</H2O>
+                            <SO2 Desc="SO2 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.4</SO2>
+                            <HC Desc="HC emitted during the LTO cycle" ToolLevel="1" Unit="kg">-2.376</HC>
+                            <CO Desc="CO emitted during the LTO cycle" ToolLevel="1" Unit="kg">2.018</CO>
+                            <NOx Desc="NOx emitted during the LTO cycle" ToolLevel="1" Unit="kg">3.831</NOx>
+                            <PM10 Desc="PM10 emitted during the LTO cycle" ToolLevel="1" Unit="kg">0.009</PM10>
+                        </LTO>
+                        <Cruise Desc="Triebwerksemissionen des Reiseflugs fuer eine (!) StudyMission">
+                            <CO2 Desc="CO2 emitted during cruise" ToolLevel="1" Unit="kg">9149.073</CO2>
+                            <H2O Desc="H2O emitted during cruise" ToolLevel="1" Unit="kg">3486.468</H2O>
+                            <SO2 Desc="SO2 emitted during cruise" ToolLevel="1" Unit="kg">2.441</SO2>
+                            <HC Desc="HC emitted during cruise" ToolLevel="1" Unit="kg">-2.055</HC>
+                            <CO Desc="CO emitted during cruise" ToolLevel="1" Unit="kg">1.349</CO>
+                            <NOx Desc="NOx emitted during cruise" ToolLevel="1" Unit="kg">7.688</NOx>
+                            <PM10 Desc="PM10 emitted during cruise" ToolLevel="1" Unit="kg">0.01</PM10>
+                        </Cruise>
+                    </Mission>
+                </OperationComponents>
+            </Operations>
+            <EndOfLife>
+                <CO2 Desc="Kohlenstoffdioxid" ToolLevel="1" Unit="kg">-114694.14</CO2>
+                <H2O Desc="Wasser" ToolLevel="1" Unit="kg">-1466106.754</H2O>
+                <NOx Desc="Stickoxide" ToolLevel="1" Unit="kg">-495.854</NOx>
+                <CO Desc="Kohlenmonoxid" ToolLevel="1" Unit="kg">-1949.608</CO>
+                <SO2 Desc="Schwefeldioxid" ToolLevel="1" Unit="kg">-1061.466</SO2>
+                <CH4 Desc="Methan" ToolLevel="1" Unit="kg">-304.18</CH4>
+                <PM10 Desc="Feinstaub" ToolLevel="1" Unit="kg">0.419</PM10>
+                <N2O Desc="Distickstoffmonoxid (Lachgas)" ToolLevel="1" Unit="kg">0</N2O>
+                <PFC Desc="Perfluoromethane und Perfluoroethane" ToolLevel="1" Unit="kg">0</PFC>
+                <NMVOC Desc="non methane volatile organic compounds" ToolLevel="1" Unit="kg">0</NMVOC>
+                <HC Desc="Kohlenwasserstoff" ToolLevel="1" Unit="kg">-3.735</HC>
+            </EndOfLife>
+        </Emissions>
+        <CED Desc="Cumulative Energy Demand">
+            <CEDTotal Desc="End-of-Life Costs" ToolLevel="1" Unit="MJ">1.033604491e+16</CEDTotal>
+            <CEDComponents>
+                <Development Desc="Development" ToolLevel="1" Unit="MJ">2.115958924e+14</Development>
+                <Production Desc="Production" ToolLevel="1" Unit="MJ">1.332765215e+13</Production>
+                <Operations Desc="Operation" ToolLevel="1" Unit="MJ">1.011292433e+16</Operations>
+                <EndOfLife Desc="End of Life" ToolLevel="1" Unit="MJ">-1.802957726e+12</EndOfLife>
+            </CEDComponents>
+        </CED>
+        <ClimateImpact Desc="Climate Impact due to Aircraft Operation">
+            <ATR Desc="Average Temperatur Response per year for aircraft operating lifetime" ToolLevel="1" Unit="mK">0.0014420111</ATR>
+            <AGTP Desc="Absolute Global Temperature Potential after final year of operation" ToolLevel="1" Unit="K">2.13271e-05</AGTP>
+            <AGTP100 Desc="Absolute Global Temperature Potential after 100 years" ToolLevel="1" Unit="K">3.52252e-05</AGTP100>
+            <AGWP Desc="Absolute Global Warming Potential after final year of operation" ToolLevel="1" Unit="(W/m2)*year">4.29914e-05</AGWP>
+            <AGWP100 Desc="Absolute Global Warming Potential after 100 years" ToolLevel="1" Unit="(W/m2)*year">0</AGWP100>
+        </ClimateImpact>
+        <AirQuality Desc="Climate Impact due to Aircraft Operation">
+            <ToleranceFactors Desc="Tolerance Factors of Emissions emitted during LTO" Unit="-">
+                <HC Desc="TF Kohlenwasserstoff" ToolLevel="1" Unit="-">-0.4355</HC>
+                <CO Desc="TF Kohlenmonoxid" ToolLevel="1" Unit="-">0.0614</CO>
+                <NOx Desc="TF Stickoxide" ToolLevel="1" Unit="-">0.1915</NOx>
+                <soot Desc="TF Russ" ToolLevel="1" Unit="-">0.0767</soot>
+            </ToleranceFactors>
+            <AirQualityIndex Desc="Air Quality Index" ToolLevel="1" Unit="-">-0.0265</AirQualityIndex>
+        </AirQuality>
+    </EcologicalValues>
+    <Requirements Desc="Designforderungen">
+        <m_Payload Desc="Design-Nutzlast (z.B. Anzahl PAX*MassPerPAX, s. DesignSpecification/Accommodation/)" Unit="kg">17000</m_Payload>
+        <m_MaximumPayload Desc="Maximale Nutzlast i. a. (PAX + 2*Luggage, da Cargo ~ Luggage)" Unit="kg">20000</m_MaximumPayload>
+        <DesignMission Desc="Definition der Auslegungsmission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
+            <R_Design Desc="Auslegungsreichweite" Unit="NM">2500</R_Design>
+            <TOFL_Design Desc="Auslegungsstartstrecke (Balanced Field Length)" Unit="m">2200</TOFL_Design>
+            <TTC_Design Desc="Auslegungs- Time-to-Climb (von 1500 ft auf ICA bei ISA+10)" Unit="min">35</TTC_Design>
+            <ClimbGradients Desc="Steiggradientenforderungen">
+                <secondTOsegment Desc="Climb gradient in 2nd take-off segment" Unit="percent">2.4</secondTOsegment>
+                <finalTOsegment Desc="Climb gradient in final take-off segment" Unit="percent">1.2</finalTOsegment>
+                <approachAEO Desc="Approach gradient with all engine operating" Unit="percent">3.2</approachAEO>
+                <approachOEI Desc="Approach gradient with one engine inoperative" Unit="percent">2.1</approachOEI>
+            </ClimbGradients>
+            <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
+                <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
+                <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+                <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+                <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
+            </ClimbSpeedSchedule>
+            <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
+                <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+                <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+            </DescentSpeedSchedule>
+            <h_initialCruise_Design Desc="Erste Cruise-Altitude (TOC)" Unit="ft">33000</h_initialCruise_Design>
+            <M_initialCruise_Design Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise_Design>
+            <LDN_Design Desc="Auslegungslandestrecke (Sicherheitslandestrecke)" Unit="m">1850</LDN_Design>
+            <V_ApproachSpeed_Design Desc="Auslegungsanfluggeschwindigkeit in KCAS, Approach Category A: 0-90 kts, B: 91-120 kts, C: 121-140 kts, D: 141-165 kts, E: greater 165 kts" Unit="KCAS">138</V_ApproachSpeed_Design>
+            <AlternateDistance Desc="Reichweite der Alternate  Mission" Unit="NM">200</AlternateDistance>
+            <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
+            <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
+            <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
+            <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
+        </DesignMission>
+        <StudyMission Desc="Definition der Study-Mission mit Startstrecke, Steigleistung, Initial Cruise und Landestrecke">
+            <R_Design Desc="Auslegungsreichweite" Unit="NM">500</R_Design>
+            <m_Payload Desc="Nutzlast auf Study-Mission" Unit="kg">13608</m_Payload>
+            <NumberOfPAX Desc="Anzahl Passagiere auf Study-Mission" Unit="-">150</NumberOfPAX>
+            <ClimbSpeedSchedule Desc="Liste der Geschwindigkeiten im Steigflug CAS unter FL100; CAS ueber FL100; M_cruise ueber Crossover-Altitude. Ggf. nur die erste bzw. die ersten beiden Geschwindigkeiten (Prop).">
+                <ClimbSpeeds Desc="Anzahl der Climb-Speed der Schedule. 1 = eine CAS, 2 = CAS mit ATC-limit u. darueber, 3 = zwei CAS u. eine Machzahl">3</ClimbSpeeds>
+                <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+                <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+                <Delta_MclimbToMcruise Desc="Differenz der Machzahl ueber Crossover-Altitude zur Cruise Machzahl" Unit="-">-0.02</Delta_MclimbToMcruise>
+            </ClimbSpeedSchedule>
+            <DescentSpeedSchedule Desc="Liste der Geschwindigkeiten im Sinkflug CAS unter FL100; CAS ueber FL100; Standardmaessig M_cruise ueber Crossover-Altitude.">
+                <CASATClimit Desc="CAS unter FL100" Unit="KCAS">250</CASATClimit>
+                <CAS Desc="CAS ueber FL100" Unit="KCAS">300</CAS>
+            </DescentSpeedSchedule>
+            <h_initialCruise Desc="Erste Cruise-Altitude (TOC)" Unit="ft">35000</h_initialCruise>
+            <M_initialCruise Desc="Erste Cruise-Machzahl (TOC)" Unit="-">0.78</M_initialCruise>
+            <AlternateDistance Desc="Reichweite der Alternate  Mission" Unit="NM">200</AlternateDistance>
+            <TakeOffProcedure Desc="Standard, ICAO-A, ICAO-B">Standard</TakeOffProcedure>
+            <ApproachProcedure Desc="Standard, CDA, CDA-Steep">Standard</ApproachProcedure>
+            <TaxiTimeOrigin Desc="Dauer des Taxiing beim Start" Unit="min">9</TaxiTimeOrigin>
+            <TaxiTimeDestination Desc="Dauer des Taxiing nach der Landung" Unit="min">5</TaxiTimeDestination>
+        </StudyMission>
+        <FuelPlanningMethod Desc="Methode zur Tankschaetzung: JAR, FAR-Domestic, FAR-Flag (International)">JAR</FuelPlanningMethod>
+        <V_MaximumGroundspeed Desc="Maximale Rollgeschwindigkeit, durch das Tyre Speed Rating begrenzt in KCAS" Unit="KCAS">195</V_MaximumGroundspeed>
+        <DesignFlightEnvelope>
+            <VMO Desc="Max operating speed. IAS also die Strukturbestimmenden Staudruckgeschwindigkeit" Unit="KCAS">350</VMO>
+            <MMO Desc="Max operating Mach No." Unit="-">0.82</MMO>
+            <h_maxOperating Desc="Max operating Altitude" Unit="ft">38500</h_maxOperating>
+            <h_maxOEI Desc="Max operating Altitude One-Engine-Inoperative" Unit="ft">15000</h_maxOEI>
+        </DesignFlightEnvelope>
+        <SizeLimits Desc="maximale geometrische Abmasse">
+            <SpanLimit Desc="Spannweitenbegrenzung" Unit="m">36</SpanLimit>
+        </SizeLimits>
+        <ACN Desc="Aircraft Classification Number">
+            <ACNCatType Desc="ACN Pavement Type; flex oder rigid" Unit="-">flex</ACNCatType>
+            <ACNCategory Desc="ACN Pavement Strength; A, B, C oder D" Unit="-">B</ACNCategory>
+            <ACNLimit Desc="ACN Limit fuer die ausgewaehlte Kategorie" Unit="-">42</ACNLimit>
+        </ACN>
+    </Requirements>
+    <DesignSpecification Desc="Spezifikation des Entwurfs">
+        <Configuration Desc="Qualitative Beschreibung der Konfiguration">
+            <Wing Desc="Parameter des Fluegels">
+                <Position Desc="Fluegellage low, mid, high" Unit="-">low</Position>
+            </Wing>
+            <Stabiliser Desc="Parameter des Hoehenleitwerks">
+                <h_OverWing Desc="Vertikale Position bzgl. des Seitenleitwerks (0: conventional 1: T-Tail)" Unit="-">0</h_OverWing>
+            </Stabiliser>
+            <LandingGear Desc="Fahrwerksanordnung">
+                <MainGearPosition Desc="Position des Hauptfahrwerks (Wing oder Fuselage)">Wing</MainGearPosition>
+                <Retractable Desc="Switch for (non-)retractable LandingGear">1</Retractable>
+            </LandingGear>
+            <Fuselage Desc="Fuselage parameters">
+                <Pressurized Desc="Is the fuselage pressurized? 1 for yes, 0 for no">1</Pressurized>
+            </Fuselage>
+            <CertificationType Desc="Zertifizierung nach CS-23 oder CS-25">CS-25</CertificationType>
+            <Fin Desc="Parameter des Seitenleitwerks">
+                <FinConfig Desc="0: Conventional 1: H-Tail" Unit="-">0</FinConfig>
+            </Fin>
+        </Configuration>
+        <Accommodation Desc="Vorgaben bezueglich der Passagierdecks und Klassen">
+            <MassPerPAX Desc="Masse pro PAX (z.B. PAX 75 kg + Luggage: Std.-Wert 90.72 kg (Quelle Airbus: All about the A320 family, Tech App.))" Unit="kg">90.72</MassPerPAX>
+            <PAXDecks Desc="Anzahl der Passagierdecks">1</PAXDecks>
+            <PAXDeck Desc="Passagierdeck mit Klassen in der Folge der Klassen-ID" ID="1">
+                <Classes Desc="Anzahl der verschiedenen Klassen auf diesem Deck">2</Classes>
+                <Class Desc="Definition der Klasse" ID="1">
+                    <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">business</ClassType>
+                    <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
+                    <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">12</Seats>
+                </Class>
+                <Class Desc="Definition der Klasse" ID="2">
+                    <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">economy</ClassType>
+                    <Seating Desc="Bestuhlung des Querschnitts">33</Seating>
+                    <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">138</Seats>
+                </Class>
+                <Class Desc="Definition der Klasse" ID="3">
+                    <ClassType Desc="Luftfahrttypische Bezeichnung der Klasse (z.B. economy, business, first)">first</ClassType>
+                    <Seating Desc="Bestuhlung des Querschnitts">22</Seating>
+                    <Seats Desc="Gesamtanzahl der Sitze in dieser Klasse">0</Seats>
+                </Class>
+            </PAXDeck>
+        </Accommodation>
+        <Cargo Desc="Vorgaben bezueglich der Frachtdecks und ULDs">
+            <CargoDecks Desc="Anzahl der Frachtdecks">1</CargoDecks>
+            <CargoDeck Desc="Cargodeck mit verschiedenen Containertypen" ID="1">
+                <Compartments Desc="Anzahl der verschiedenen Compartments auf diesem Deck">2</Compartments>
+                <Compartment Desc="Definition des Compartments" ID="1">
+                    <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">forward</CompartmentType>
+                    <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
+                    <ULDType Desc="Definition der Containergruppe" ID="1">
+                        <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
+                        <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
+                        <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">3</ULDs>
+                    </ULDType>
+                </Compartment>
+                <Compartment Desc="Definition des Compartments" ID="2">
+                    <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">aft</CompartmentType>
+                    <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
+                    <ULDType Desc="Definition der Containergruppe" ID="1">
+                        <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
+                        <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
+                        <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">4</ULDs>
+                    </ULDType>
+                </Compartment>
+                <Compartment Desc="Definition des Compartments" ID="3">
+                    <CompartmentType Desc="Luftfahrtypische Bezeichnung des Compartments (z.B. forward, aft, bulk)">bulk</CompartmentType>
+                    <ULDTypes Desc="Anzahl der verschiedenen Containergruppen auf diesem Deck">1</ULDTypes>
+                    <ULDType Desc="Definition der Containergruppe" ID="1">
+                        <ULD Desc="Normbezeichnung des ULD">LD3-45</ULD>
+                        <ULDInRow Desc="Anzahl der ULDs in einer Rumpfsektion">1</ULDInRow>
+                        <ULDs Desc="Gesamt Anzahl dieser ULDs diesen Types auf diesem Deck">1</ULDs>
+                    </ULDType>
+                </Compartment>
+            </CargoDeck>
+        </Cargo>
+        <Propulsion Desc="Vorgaben zum Antriebssystem">
+            <TypeOfEngine Desc="Triebwerkstechnologie (Jet oder Prop)" Unit="-">Jet</TypeOfEngine>
+            <NumberOfEngines Desc="Anzahl der Triebwerke">2</NumberOfEngines>
+            <PositionOfEngines Desc="Positionierung der Triebwerke">
+                <EnginesOnWing Desc="Anzahl der Triebwerke am Fluegel">2</EnginesOnWing>
+                <EnginesOnFuselage Desc="Anzahl der Triebwerke am Rumpf, mit Pylons montiert">0</EnginesOnFuselage>
+                <EnginesInFuselage Desc="Anzahl der Triebwerke im Rumpf integriert">0</EnginesInFuselage>
+                <WingEnginePosition Desc="0=EngineUnderWing; 1= EnginesOverWing">0</WingEnginePosition>
+            </PositionOfEngines>
+            <FuelDensity Desc="Dichte des Kraftstoffs" Unit="kg/l">0.785</FuelDensity>
+        </Propulsion>
+        <TankConfiguration Desc="Vorgaben zur Aufteilung der Tanks">
+            <NumberOfCenterTanks Desc="Anzahl der Tanks im Rumpf (Fluegelkasten + zus. Tanks)">1</NumberOfCenterTanks>
+            <NumberOfWingTanks Desc="Anzahl der Tanks im Fluegel">2</NumberOfWingTanks>
+            <NumberOfTrimTanks Desc="Anzahl der Tanks zur Trimmung">0</NumberOfTrimTanks>
+        </TankConfiguration>
+        <HighLiftSystem Desc="Vorgaben zum Hochauftriebssystem">
+            <C_LmaxT-O Desc="Maximaler Auftriebsbeiwert in Startkonfiguration. Statistik, falls Wert 0" Unit="-">2.3</C_LmaxT-O>
+            <C_LmaxLanding Desc="Maximaler Auftriebsbeiwert in Landekonfiguration. Statistik, falls Wert 0" Unit="-">2.8</C_LmaxLanding>
+        </HighLiftSystem>
+        <DesignLoads Desc="Vorgaben zu zulaessigen Lastvielfachen">
+            <n1 Desc="maximum positive load limit (CS-25: n1=2.5g)" Unit="g">2.5</n1>
+            <n2 Desc="maximum negative load limit (CS-25: n2=-1.0g)" Unit="g">-1</n2>
+        </DesignLoads>
+        <Technology Desc="Vorgaben spezieller Technologien">
+            <LaminarFlow Desc="HLFC oder NLF">
+                <Components Desc="Flugzeugkomponenten, auf die HLFC/NLF angewendet wird">
+                    <Wing>
+                        <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
+                        <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
+                    </Wing>
+                    <Stabilizer>
+                        <UpperSide Desc="Fluegeloberseite (HLFC, NLF, None)">None</UpperSide>
+                        <LowerSide Desc="Fluegelunterseite (HLFC, NLF, None)">None</LowerSide>
+                    </Stabilizer>
+                    <Fin Desc="Seitenleitwerk (HLFC, NLF, None)">None</Fin>
+                    <Nacelles Desc="Triebwerksgondeln (HLFC, NLF, None)">None</Nacelles>
+                </Components>
+            </LaminarFlow>
+            <ElectricTaxiing>
+                <DoElectricTaxiing Desc="1: Electric Taxiing, 0: Propulsion Taxiing">0</DoElectricTaxiing>
+                <EngineWarmupTime Desc="Laufzeit der Triebwerke vor dem Start" Unit="min">0</EngineWarmupTime>
+            </ElectricTaxiing>
+            <BallisticRecoverySystem Desc="Ballistic Recovery System (Parachute)">0</BallisticRecoverySystem>
+        </Technology>
+    </DesignSpecification>
+</AcftExchangeFile>