Bombardier Challenger 850
Challenger 800 / 850 | |
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Challenger 850 taking off | |
Role | Business jet |
Manufacturer | Bombardier Aerospace |
First flight | 30 August 2006 |
Status | Active |
Primary user | AirX Charter |
Produced | 2006-2015[1] |
Developed from | Bombardier CRJ200 |
The Bombardier Challenger 800 was the largest super-midsize business jet offered by Bombardier Aerospace. It is based on Bombardier's 50-seat Bombardier CRJ200 LR. The Challenger 850 was the updated version, produced from 2006 to 2015. This aircraft is no longer for sale.[2]
Design and development[]
![](http://upload.wikimedia.org/wikipedia/commons/thumb/c/ce/OD-TAL_Canadair_CRJ.100LR_Interior_%287608260732%29.jpg/220px-OD-TAL_Canadair_CRJ.100LR_Interior_%287608260732%29.jpg)
corporate interior
The Challenger 850 is derived from the Bombardier CRJ200 airliner. It is capable of accommodating 12–16 passengers. The Challenger 850 jet has a transcontinental range and a high-speed cruise of Mach 0.80.
Specifications[]
Data from Bombardier website[3]
General characteristics
- Crew: 2 + 1
- Capacity: up to 16
- 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 (9,217 lbf) for take=off in ISA + 8°C (73°F)
Performance
- Maximum speed: Mach (Vmo) 0.850
- Cruise 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
- (Theoretical range with NBAA IFR Reserves, ISA, 8 pax/2 crew. Actual range will be affected by speed, weather, selected options and other factors.)
- Service ceiling: 12,500 m (41,000 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
- 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[]
Related development
- Bombardier CRJ200
- Bombardier Global 6000
- Bombardier Challenger 600
- Bombardier Challenger 300
Related lists
References[]
- ^ "Bombardier Challenger 850". 2016-05-13.
- ^ "Discover our jets".
- ^ "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[]
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Wikimedia Commons has media related to Bombardier Challenger 850. |
Categories:
- Bombardier Aerospace aircraft
- 1990s Canadian business aircraft
- Twinjets
- T-tail aircraft
- Aircraft first flown in 2006