Specifications - Bombardier Challenger 604 Intercontinental Business Jet, Canada
| Dimensions | |
|---|---|
| Crew | 2+1 |
| Passengers | 9 business class or up to 19 with high density interior |
| Length | 20.85m |
| Wingspan | 19.61m |
| Wing area | 45.71m |
| Height | 6.30m |
| Maximum fuselage diameter | 2.69m |
| Turning circle | 12.19m |
| Cabin Dimensions | |
| Cabin length, excluding cockpit | 8.66m |
| Cabin width | 2.49m |
| Floor level cabin width | 2.18m |
| Maximum height | 1.85m |
| Cabin floor area | 18.77m² |
| Cabin volume | 32.56m³ |
| Weights | |
| Maximum ramp weight | 21,636kg |
| Maximum take-off weight | 21,591kg |
| Maximum landing weight | 17,237kg |
| Maximum zero fuel weight | 14,515kg |
| Basic operating weight | 12,079kg |
| Maximum fuel load | 9,072kg |
| Maximum payload | 2,436kg |
| Payload with full fuel | 485kg |
| Engines | |
| Turbofan engines | 2 General Electric CF34-3B |
| Power | 38.84kN (8,729lb) thrust at take-off |
| Performance | |
| Maximum range (5 pax, 2 crew, max fuel) | 7,551km (4,077nm) |
| High speed cruise | 870km/h |
| Normal cruise speed | 850km/h |
| Long range cruise speed | 787km/h |
| Maximum operating altitude | 12,497m (41,000ft) |
| Initial cruise altitude | 11,430m (37,500ft) |
| Time to initial cruise altitude | 22min |
| Fuel consumption at average cruise | 1,192l/hr |
| Balanced field length, SL,ISA MTOW | 1,738m |
| Landing distance at maximum landing weight | 846m |
| Noise level, take-off | 80.9 EPNdB |
| Noise level, sideline | 90.3 EPNdB |
| Noise level, approach | 86.2 EPNdB |
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