Bombardier Challenger 850
From Wikipedia, the free encyclopedia
The Bombardier Challenger 800 is the largest super-mid size business aircraft offered by Bombardier Aerospace. It is based on Bombardier's 50-seat CRJ200LR. The Challenger 850 is the updated, current version.
[edit] Design and development
The Challenger 850 is derived from the Bombardier CRJ200 airliner. It is capable of accommodating 15-19 passengers. The Challenger 850 jet has a transcontinental range and a high-speed cruise of Mach 0.80.
The average price for the Challenger 850 is $31.862 million.
[edit] Specifications
Data from http://www2.bombardier.com/en/3_0/3_2/3_2_2/3_2_2_3_3.jsp?pageid=3_2
General characteristics
- Crew: 2 + 1
- Capacity: 15 to 19 passengers
- Length: 87.83 ft (26.77 m)
- Wingspan: 69.58 ft (21.21 m)
- Height: 20.42 ft (6.22 m)
- Wing area: 520.4 ft2 (48.35 m2)
- Empty weight: 34,790 lb (15,780 kg)
- Useful load: 18,210 lb (8,261 kg)
- Max. takeoff weight: 53,250 lb (24,041 kg)
- Powerplant: 2 × General Electric CF34-3B1 turbofan engines, 8,729 lbf (38.84 kN) each
Performance
- Cruise speed: 442 kts (819 km/h)
- Range: 2,811 nm (5,206 km)
- Service ceiling: 41,000 ft (12,497 m)
- Balanced field length (SL, ISA, MTOW): 6,305 ft (1,922 m)
- Landing distance (SL, ISA, MLW): 2,910 ft (887 m)
- Noise Level (EPNdB): Flyover: 78.8, Approach: 92.1, Lateral: 82.4
[edit] See also
- Related development
- Related lists
[edit] References
The initial version of this article was based on a public domain article from Greg Goebel's Vectorsite.
[edit] External links
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