Bombardier Challenger 850 Specifications
Below are the Bombardier Challenger 850 Specifications.
Challenger 850 Specifications – General:
- Capacity: Crew: 2 + Typical seating: Up to 14 = 16 total persons
Challenger 850 Specifications – Engines:
- General Electric CF34-3B1 turbofans
- Thrust: 8,729 lb (38.84 kN)
- Thrust with APR: 9,220 lb (41.0 kN)
- Flat rated to: ISA + 8°C (73°F)
Challenger 850 Avionics Specifications:
- Rockwell Collins Pro Line 4
- six-screen EFIS
- Two-screen EICAS
- Dual Flight Management System (FMS) 4200
- Dual Global Positioning System (GPS)
- Dual Inertial Reference System (IRS)
- Dual DME / Dual ADF
- Enhanced Ground Proximity Warning
- System (EGPWS)
- Traffic Collision Avoidance System (TCAS II)
Bombardier Challenger 850 Performance Specifications:
- Challenger 850 Range with 8 passengers: 2,811 nm 3,235 sm or 5,206 km (NBAA IFR Reserves, ISA,
- 8 pax/2 crew).
- Bombardier Challenger 850 Speed:
- High-speed 459 Knots 528 mph 850 km/h 0.80 Mach
- Typical cruise speed: 442 Knots 509 mph 819 km/h 0.77 Mach
- Long-range speed: 425 Knots 489 mph 787 km/h 0.74 Mach
Challenger 850 Specifications - Airfield Performance:
- Takeoff distance: 6,305 ft (1,922 m) (SL, ISA, MTOW).
- Landing distance: 2,910 ft (887 m) (SL, ISA, MLW)
Operating Altitude
- Maximum operating altitude: 41,000 ft (12,497 m)
Noise Level (EPNdB)
- Flyover: 78.8
- Approach: 92.1
- Lateral: 82.4
Bombardier Challenger 850 Dimensions: See our Challenger 850 Dimensions Page
Bombardier Challenger 850 Weights:
- Maximum ramp weight: 53,250 lb (24,154 kg)
- Maximum takeoff weight: 53,000 lb (24,040 kg)
- Maximum landing weight: 47,000 lb (21,319 kg)
- Maximum zero fuel weight: 44,000 lb (19,958 kg)
- Typical basic operating weight: 34,618 lb (15,702 kg)
- Maximum usable fuel weight: 18,274 lb (8,289 kg)
- Maximum payload (D-E): 9,382 lb (4,256 kg)
- Payload - maximum fuel (A-E-F): 358 lb (162 kg)
- Fuel with maximum payload (A-D): 9,250 lb (4,196 kg)
Above Challenger 850 Photo by Konflikty. pl on Wikimedia Commons.