Aircraft Performance
| Weights (lb) | Challenger 601-3R, CL-600-2B16 | |||
|---|---|---|---|---|
| Max Ramp | 45,250 | |||
| Max Takeoff | 45,100 | |||
| Max Landing | 36,000 | |||
| Zero Fuel | 31,000c | |||
| BOW | 26,250 | |||
| Max Payload | 4,750 | |||
| Useful Load | 19,000 | |||
| Executive Payload | 2,200 | |||
| Max Fuel | 17,655 | |||
| Max Fuel | 17,655 | |||
| Avail Payload Max Fuel | 1,345 | |||
| Avail Fuel Max Payload | 14,250 | |||
| Avail Fuel Exec Payload | 16,800 | |||
| Limits | Challenger 601-3R, CL-600-2B16 | |||
| MMO | 0.850 | |||
| Transition Altitude FL/VMO | FL 213/360 | |||
| Cabin Pressurization (PSI) | 8.8 | |||
| Airport Performance | Challenger 601-3R, CL-600-2B16 | |||
| TO (Sea Level, ISA Temp) | 6,050 | |||
| TO (5000′, @25C) | 11,094 | |||
| Hot/High WAT | 45,100 | |||
| NBAA IFR Ranges V2 @ SL ISA, MTOW |
3,510 148 |
|||
| VREF | 120 | |||
| Landing Distance with 4 Passengers | 2,785 | |||
| Climb | Challenger 601-3R, CL-600-2B16 | |||
| Time to Climb/Alt | N/A | |||
| Engine Out Rate fpm | 1,180 | |||
| FAR 25 Engine-Out Grad (ft/nm) | 414 | |||
| Ceilings (ft) | Challenger 601-3R, CL-600-2B16 | |||
| Certificated | 41,000 | |||
| All Eng Srv | 38,100 | |||
| Eng Out Service | 25,000 | |||
| Sea Level Cabin | 23,200 | |||
| Long Range Cruise | Challenger 601-3R, CL-600-2B16 | |||
| KTAS | 425 | |||
| Fuel Flow | 1,700 | |||
| Altitude | FL 410 | |||
| Specific Range | 0.250 | |||
| High Speed Cruise | Challenger 601-3R, CL-600-2B16 | |||
| KTAS | 459 | |||
| Fuel Flow | 1,921 | |||
| Altitude | FL 410 | |||
| Specific Range | 0.239 | |||
| Data based on latest manufactured year | ||||