| Convergence successful | |
| Postprocessing not successful | |
| Needed time | 0.02 min |
| Number of iterations | 1 |
| MTOM [kg]: | 78619.9 |
| OME [kg]: | 42154.3 |
| Max. Usable Fuel [kg]: | 32177.4 |
| Loaded Fuel on Design Mission [kg]: | 19566.5 |
| TLAR | Unit | Requirement | Calc | Rel. Change [%] | Fulfilled | Checked | Recommendation |
|---|---|---|---|---|---|---|---|
| Balanced Field Length (BFL) @ SL, MTOM, ISA+0-Conditions | m | < 2122 | 0 | -100 | 1 | 0 | |
| Landing distance (LDN) @ MLM, SL, ISA+0 | m | < 2387 | 1353.28 | -43.31 | 1 | 0 | |
| Approach speed (v_app) | KCAS | < 138 | 128.745 | -6.71 | 1 | 0 | |
| Initial Cruise Altitude (ICA) after T/O @ MTOM, ISA+0 | ft | 33000 | 33000 | 0 | 1 | 0 | |
| Time-to-climb (TTC) after T/O @ MTOM, ISA+0 (from 1500 ft to ICA) | min | < 35 | 15.83 | -54.77 | 1 | 0 | |
| Max. operating (cruise) altitude Climb with 100 ft/min @ ISA+0 | ft | > 38500 | 35000 (38790.1) | 0.75 | 1 | 0 | |
| Max. ceiling Climb with 50 ft/min @ ISA+0 | ft | - | 38945.9 | - | - | - | |
| One-engine-out (OEI) net ceiling Climb with 100 ft/min @ ISA+0 | ft | > 15000 | 21589.8 | 43.93 | 1 | 0 | |
| (Initial) Cruise Mach number | - | 0.78 | 0.78 | 0 | 1 | 0 | |
| 2nd (T/O) Segment Climb Grad. | % | > 2.4 | 2.40917 | 0.38 | 1 | 0 | |
| Final (T/O) Segment Climb Grad. | % | > 1.2 | 2.40917 | 100.76 | 1 | 0 | |
| Approach Gradient (OEI) | % | 2.1 | - | - | 1 | 0 | |
| Approach Gradient (AEO) | % | 3.2 | - | - | 1 | 0 |
| Parameter | Unit | Req. Value |
|---|---|---|
| Design range | NM | 2500 |
| Design payload [200 lb (=90.72 kg) per PAX] | kg | 17000 |
| Maximum payload | kg | 20000 |
| (Initial) cruise Mach number | - | 0.78 |
| Max. operating Mach number (MMO) | kg | 0.82 |
| Max. operating speed (VMO) | kg | 350 |
| Initial Cruise Altitude (ICA) after T/O @ MTOM, ISA+0 | ft | 33000 |
| Time-to-climb (TTC) after T/O @ MTOM, ISA+0 (from 1500 ft to ICA) | min | < 35 |
| One-engine-out (OEI) net ceiling Climb with 100 ft/min @ ISA+0 | ft | > 15000 |
| Max. operating (cruise) altitude Climb with 100 ft/min @ ISA+0 | ft | > 38500 |
| Balanced Field Length (BFL) @ SL, MTOM, ISA+0 | m | < 2122 |
| Landing distance (LDN) @ MLM, SL, ISA+0 | m | < 2387 |
| Approach speed (v_app) | KCAS | < 138 |
| Wing span limit | m | ≤ 36 |
| ACN (flex B) | - | < 42 |
| Parameter | Symbol | Unit | Value |
|---|---|---|---|
| Design range | R | NM | 2500 |
| Design passenger capacity | PAX | 150 | |
| Cruise Mach number | MaCr | - | 0.78 |
| Wing loading | W/S | kg/m2 | 625.8 |
| Thrust-to-weight ratio | T/W | - | 0.332 |
| Maximum take-off mass | MTOM | t | 78.6 |
| Maximum landing mass | MLM | t | 66.3 |
| Operating mass empty | OME | t | 42.2 |
| Manufacturer's mass empty | MME | t | 38.8 |
| Maximum zero fuel mass | MZFM | t | 62.2 |
| Maximum fuel mass | MFM | t | 32.2 |
| Wing area | Sref | m2 | 125.624 |
| Wing span | b | m | 34.546 |
| Mean aerodynamic chord | MAC | m | 4.38782 |
| Engine type | - | 2 x V2527-A5 | |
| Sea-level static thrust | SLST | lbf / kN | 28778 / 128.009 |
| Iteration # | MTOM | OME | xCG | missionFuel | ||||
| abs | rel | abs | rel | abs | rel | abs | rel | |
| Start values from Aircraft XML... | ||||||||
| 0 | 78619.9 | 42154.3 | 16.8894 | 19566.5 | ||||
| ... after Setup Steps: | ||||||||
| 0 | 78619.9 | 42154.3 | 16.8894 | 19566.5 | ||||