Challenger 850

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Overview

The phenomenal Bombardier Challenger 850 aircraft is so well designed and constructed, it sets the standard for reliability, dependability and value in its class

The space and flexibility to meet all your needs
Strength and reliability standards that challenge all others
Airframe proven in over 6 million hours of commercial service

Technical Specifications

Capacity

Crew: 2 + 1

Passengers: Up to 14

Dimensions

Exterior

Length:

87.83 ft

26.77 m

Wingspan:

69.58 ft

21.21 m

Wing area (basic):

520.4 ft²

48.35 m²

Height overall:

20.42 ft

6.22 m

Interior

Cabin length:
(From cockpit divider to end of pressurized compartment)

48.42 ft

14.76 m

Cabin maximum width: (Centerline)

8.17 ft

2.49 m

Cabin width: (Floorline)

7.17 ft

2.19 m

Cabin height:

6.08 ft

1.85 m

Floor area: (Excluding cockpit)

346 ft²

32.14 m²

Cabin volume:
(Excluding cockpit)

1,990 ft³

56.36 m³

Weights

A. Maximum ramp weight:

53,250 lb

24,154 kg

B. Maximum takeoff weight

53,000 lb

24,040 kg

C. Maximum landing weight

47,000 lb

21,319 kg

D. Maximum zero fuel weight:

44,000 lb

19,958 kg

E. Typical basic operating weight:

34,618 lb

15,702 kg

F. Maximum zero fuel weight:

18,274 lb

8,289 kg

Maximum payload (D-E):

9,382 lb

4,256 kg

Payload – full fuel (A-E-F):

358 lb

162 kg

Fuel with maximum payload (A-D):

9,250 lb

4,196 kg

Performance

Range

Maximum range at M 0.74:

2,811 NM

3,235 SM

5,206 km

(Theoretical range with NBAA IFR Reserves, ISA, 8 pax/2 crew. Actual range will be affected by speed, weather, selected options and other factors.)

Speed	Mach	kt	mph	km/h
High-speed cruise	0.80	459	528	850
Typical cruise speed	0.77	442	509	819
Long-range cruise speed	0.74	425	489	787

Range Map - Beijing Hong Kong

Download Factsheet

Airfield Performance

Takeoff distance:

6,305 ft

1,922 m

(SL, ISA, MTOW)

Landing distance:

2,910 ft

887 m

(SL, ISA, MTOW)

Operating Altitude

Maximum operating altitude:

41,000 ft

12,497 m

Noise Level	Flyover	Approach	Lateral
(EPNdB)	78.8	92.1	82.4

Engines

General Electric CF34-3B1 turbofans

Thrust: 8,729 pounds (38.84 kN) thrust at takeoff

9,220 pounds (41.0 kN) thrust APR

Flat-rating: ISA + 8°C (73°F)

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)