Definitions and additional explanations can be found under: Parameter Definitions
Top-Level Aircraft Requirements:
| Parameter | Unit | Req. Value |
|---|---|---|
| Design range | NM | 2750 |
| Design payload [200 lb (=90.72 kg) per PAX] | kg | 13608 |
| Maximum payload | kg | 20000 |
| (Initial) cruise Mach number | - | 0.78 |
| Max. operating Mach number (MMO) | - | 0.82 |
| Max. operating speed (VMO) | KCAS | 350 |
| Initial Cruise Altitude (ICA) after T/O @ MTOW, ISA+10 | ft | 33000 |
| Time-to-climb (TTC) after T/O @ MTOW, ISA+10 (from 1500 ft to ICA) | min | < 35 |
| One-engine-out (OEI) net ceiling Climb with 100 ft/min @ ISA | ft | > 15000 |
| Max. operating (cruise) altitude Climb with 100 ft/min @ ISA | ft | > 38500 |
| Take-off Field Length (TOFL) @ SL, ISA+15 | m | < 2200 |
| Landing distance (LDN) @ MLW, SL, ISA | m | < 1850 |
| Approach speed (vapp,ldg) | KCAS | < 138 |
| Wing span limit | m | ≤ 36 |
| ACN (flex B) | - | < 42 |