Performance data can be downloaded here: Simulation Results of Standard Payload Passenger (SPP) Study Mission (150 PAX, 500 NM): CSR 01 MissionStudy R926 PL13608 Out
| Parameter | Comment | Unit | Value |
|---|---|---|---|
| Mission specifications | |||
| Range | NM | 500 | |
| Payload (PL) | kg | 13608 | |
| Cruise Mach number | - | 0.78 | |
| Cruise climb steps | ft | 2000 | |
| Climb Mach number | above crossover altitude | - | 0.76 |
| CAS above FL100 | KCAS | 300 | |
| CAS below FL100 | KCAS | 250 | |
| Taxi-out time | min | 9 | |
| Taxi-in time | min | 5 | |
| Alternate distance | NM | 200 | |
| Fuel reserves method | JAR-OPS 1.255 | ||
| Mission simulation results | |||
| Take-off weight | TOW = OWE + PL + MF - TXFout | kg | 62089 |
| Mission (loaded) fuel | MF = BF + RF | kg | 6665 |
| Block fuel | BF = TF + TXFout + TXFin | kg | 3765 |
| Trip fuel | TF | kg | 3337 |
| Reserve fuel | RF | kg | 2900 |
| Taxi-out fuel | TXFout | kg | 276 |
| Taxi-in fuel | TXFin | kg | 153 |
| Landing weight | LW = MTOW - TF | kg | 58753 |
| Block time | h | 1.55 | |
| Flight time | h | 1.31 | |
Note: the small CL peak at the very beginning of the cruise phase is due to the acceleration phase from climb Mach number (Ma 0.76) to initial cruise Mach number (Ma 0.78).