Bombardier Challenger 850
| Challenger 800 / 850 | |
|---|---|
 | |
| Challenger 850 C-GWWW at Manchester May 2008 | |
| Role | Business jet |
| Manufacturer | Bombardier Aerospace |
| First flight | 30 August 2006 |
| Status | Active, In production |
| Produced | 2006-present |
| Unit cost | |
| Developed from | Bombardier CRJ200 |
The Bombardier Challenger 800 is the largest super-midsize business aircraft offered by Bombardier Aerospace. It is based on Bombardier's 50-seat CRJ200LR. The Challenger 850 is the updated, current version.
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.
Specifications
Data from Bombardier website[2]
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 (9,217 lbf) 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
- (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 (41,010 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
- Related development
- Related lists
References
- ↑ "Business Airplanes" (PDF). Business & Commercial Aviation. Aviation Week. May 2013.
- ↑ "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
 |
Wikimedia Commons has media related to Bombardier Challenger 850. |
This article is issued from Wikipedia - version of the 11/5/2016. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.