Bombardier Challenger 850
From Wikipedia, the free encyclopedia
| Challenger 800 / 850 | |
|---|---|
| Challenger 850 C-GWWW at Manchester May 2008 | |
| Role | Business jet |
| Manufacturer | Bombardier Aerospace |
| Status | In production |
| Unit cost | US$32 million |
| Developed from | Bombardier CRJ200 |
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.
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Design and development [edit]
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.
Specifications [edit]
Data from Bombardier website[1]
General characteristics
- Crew: 2 + 1
- Capacity: up to 14
- Length: 26.77 m (87 ft 10 in)
- Wingspan: 21.21 m (69 ft 7 in)
- Height: 6.22 m (20 ft 5 in)
- Wing area: 48.35 m2 (520.4 sq ft)
- Empty weight: 15,440 kg (34,039 lb)
- Maximum ramp weight: 24,154 kg (53,250 lb)
- Maximum takeoff weight: 24,040 kg (52,999 lb)
- Maximum landing weight: 21,319 kg (47,000 lb)
- Maximum zero fuel weight: 19,958 kg (44,000 lb)
- Typical basic operating weight: 15,702 kg (34,617 lb)
- Maximum usable fuel weight: 8,289 kg (18,274 lb)
- Maximum payload (D-E): 4,256 kg (9,383 lb)
- Payload – full fuel (A-E-F): 162 kg (357 lb)
- Fuel with maximum payload (A-D): 4,196 kg (9,251 lb)
- Powerplant: 2 × General Electric CF34-3B1 turbofan engines, 38.84 kN (8,730 lbf) thrust each 41 kN (90,390 lb) for take=off in ISA + 8°C (73°F)
Performance
- Maximum speed: Mach (Vmo) 0.850
- Cruising speed: 819 km/h (509 mph; 442 kn)
- High-speed cruise: M0.80 / 850 km/h (528 mph)
- Long-range cruise speed: M0.74 / 787 km/h (489 mph)
- Range: 5,206 km (3,235 mi; 2,811 nmi) at M 0.74
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- (Theoretical range with NBAA IFR Reserves, ISA, 8 pax/2 crew. Actual range will be affected by speed, weather, selected options and other factors.)
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- Service ceiling: 12,500 m (41,010 ft)
- Balanced field length (SL, ISA, MTOW): 6,305 ft (1,922 m)
- Landing distance (SL, ISA, MLW): 2,910 ft (887 m)
- Noise Level: Flyover: 78.8, Approach: 92.1, Lateral: 82.4 (EPNdB)
Avionics
- Rockwell Collins Pro Line 4 six-screen EFIS
- Two-Screen EICAS
- Dual FMS 4200
- Dual GPS
- Dual IRS
- Dual DME/ Dual ADF
- Enhanced Ground Proximity Warning System (EGPWS)
- Traffic Collision Avoidance System (TCAS II)
See also [edit]
- Related development
- Related lists
References [edit]
- ^ "Bombardier Challenger 850 Specifications". Canada: bombardier.com. Retrieved 6 April 2012.
- The initial version of this article was based on a public domain article from Greg Goebel's Vectorsite.
External links [edit]
| Wikimedia Commons has media related to: Bombardier Challenger 850 |
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