Aircraft Performance
| Weights (lb) | Premier I, RA-390 | |||
|---|---|---|---|---|
| Max Ramp | 12,590 | |||
| Max Takeoff | 12,500 | |||
| Max Landing | 11,600 | |||
| Zero Fuel | 10,000c | |||
| BOW | 8,500 | |||
| Max Payload | 1,500 | |||
| Useful Load | 4,090 | |||
| Executive Payload | 1,200 | |||
| Max Fuel | 3,670 | |||
| Avail Payload Max Fuel | 420 | |||
| Avail Fuel Max Payload | 2,590 | |||
| Avail Fuel Exec Payload | 2,890 | |||
| Limits | Premier I, RA-390 | |||
| MMO | 0.800 | |||
| Transition Altitude FL/VMO | FL280/320 | |||
| Cabin Pressurization (PSI) | 8.4 | |||
| Airport Performance | Premier I, RA-390 | |||
| TO (Sea Level, ISA Temp) | 3,792 | |||
| TO (5000′, @25C) | 6,888 | |||
| Hot/High WAT | 12,500 | |||
| NBAA IFR Ranges V2 @ SL ISA, MTOW |
1,178 118 |
|||
| VREF | 111 | |||
| Landing Distance with 4 Passengers | 2,975 | |||
| Climb | Premier I, RA-390 | |||
| Time to Climb/Alt | 17/FL370 | |||
| Engine Out Rate fpm | 586 | |||
| FAR 25 Engine-Out Grad (ft/nm) | 298 | |||
| Ceilings (ft) | Premier I, RA-390 | |||
| Certificated | 41,000 | |||
| All Eng Srv | 41,000 | |||
| Eng Out Service | 28,000 | |||
| Sea Level Cabin | 21,400 | |||
| Long Range Cruise | Premier I, RA-390 | |||
| KTAS | 369 | |||
| Fuel Flow | 662 | |||
| Altitude | FL 410 | |||
| Specific Range | 0.557 | |||
| High Speed Cruise | Premier I, RA-390 | |||
| KTAS | 451 | |||
| Fuel Flow | 1,203 | |||
| Altitude | FL 330 | |||
| Specific Range | 0.375 | |||
| Data based on latest manufactured year | ||||