Aircraft Performance
| Weights (lb) | Challenger 600, CL-600-1A11 | |||
|---|---|---|---|---|
| Max Ramp | 41,250 | |||
| Max Takeoff | 41,100 | |||
| Max Landing | 36,000 | |||
| Zero Fuel | 31,000c | |||
| BOW | 23,170 | |||
| Max Payload | 7,830 | |||
| Useful Load | 18,080 | |||
| Executive Payload | 1,800 | |||
| Max Fuel | 14,900 | |||
| Max Fuel | 14,900 | |||
| Avail Payload Max Fuel | 3,180 | |||
| Avail Fuel Max Payload | 10,250 | |||
| Avail Fuel Exec Payload | 14,900 | |||
| Limits | Challenger 600, CL-600-1A11 | |||
| MMO | 0.850 | |||
| Transition Altitude FL/VMO | FL 214/360 | |||
| Cabin Pressurization (PSI) | 9.3 | |||
| Airport Performance | Challenger 600, CL-600-1A11 | |||
| TO (Sea Level, ISA Temp) | 5,700 | |||
| TO (5000′, @25C) | 7,350 | |||
| Hot/High WAT | 36,200 | |||
| NBAA IFR Ranges V2 @ SL ISA, MTOW |
2,280 143 |
|||
| VREF | 117 | |||
| Landing Distance with 4 Passengers | 2,538 | |||
| Climb | Challenger 600, CL-600-1A11 | |||
| Time to Climb/Alt | N/A | |||
| Engine Out Rate fpm | 900 | |||
| FAR 25 Engine-Out Grad (ft/nm) | 277 | |||
| Ceilings (ft) | Challenger 600, CL-600-1A11 | |||
| Certificated | 41,000 | |||
| All Eng Srv | 37,000 | |||
| Eng Out Service | 15,000 | |||
| Sea Level Cabin | 25,000 | |||
| Long Range Cruise | Challenger 600, CL-600-1A11 | |||
| KTAS | 425 | |||
| Fuel Flow | 1,710 | |||
| Altitude | FL 430 | |||
| Specific Range | 0.249 | |||
| High Speed Cruise | Challenger 600, CL-600-1A11 | |||
| KTAS | 443 | |||
| Fuel Flow | 1,910 | |||
| Altitude | FL 390 | |||
| Specific Range | 0.232 | |||
| Data based on latest manufactured year | ||||