diff --git a/docs/documentation/sizing/systems_design/getting-started.md b/docs/documentation/sizing/systems_design/getting-started.md
index 204d27b4867761580f557d63ff2e019d741f0c2e..b91d9b5478a030359d141be7a93e4cee468e0a4e 100644
--- a/docs/documentation/sizing/systems_design/getting-started.md
+++ b/docs/documentation/sizing/systems_design/getting-started.md
@@ -18,6 +18,9 @@ The following will happen:
 - a HTML report is created in the directory of `aircraft_exchange_file_directory` (no plots if they are turned off)
 - results are saved in the _acXML_ file
 
+!!! note 
+    An A320-like system architecture is implemented in the provided default config file. This architecture and its system parameters will be used if you make no other changes to the config file than those stated in 2. or just run the workflow without adapting the config file of systems_design.
+
 ## Settings and outputs
 
 Three input files are required for **systems_design**:
diff --git a/docs/documentation/sizing/systems_design/systems.md b/docs/documentation/sizing/systems_design/systems.md
index 4a83ccf3259465ce884a48a494152b8d1827678f..0ee3415fdd49e72766007aee453d167846ecf2fc 100644
--- a/docs/documentation/sizing/systems_design/systems.md
+++ b/docs/documentation/sizing/systems_design/systems.md
@@ -59,6 +59,9 @@ Furnishing system includes the power required for the galleys and the inflight e
 
 Power calculation is done based on user inputs.
 
+!!! important
+    Because the mass of furnishing items is already calculated in **fuselage_design**, it is not changed in systems_design and there is no scaling factor available in systems_design to adapt this mass. If you wish to make adaptions, you can do this in [**fuselage_design**](../fuselage_design/getting_started.md/#accommodation-definitions).
+
 **Required Input Parameters**
 
 * Galley Load Fraction during Takeoff [-]: