Challenger 605

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Overview

The Bombardier Challenger 605 corporate aircraft is the next step in the continuing evolution of the world's best selling family of large business jets

Combining superior strength, versatility and reliability with cost efficiency
The edge in cockpit technology and the proven success of mature systems
A new look, feel and functionality to the widest cabin in its class

Technical Specifications

Capacity

Crew: 2

Passengers: Up to 12

Dimensions

Exterior

Length:

68.42 ft

20.85 m

Wingspan:

64.33 ft

19.16 m

Wing area (basic):

492 ft²

45.71 m²

Height overall:

20.67 ft

6.30 m

Interior

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

28.42 ft

8.66 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)

202 ft²

18.77 m²

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

1,150 ft³

32.56 m³

Weights

A. Maximum ramp weight:

48,300 lb

21,909 kg

B. Maximum takeoff weight:

48,200 lb

21,863 kg

C. Maximum landing weight:

38,000 lb

17,237 kg

D. Maximum zero fuel weight:

32,000 lb

14,515 kg

E. Typical basic operating weight:

26,915 lb

12,208 kg

F. Maximum fuel weight:

20,000 lb

9,072 kg

Payload – full fuel (A-E-F):

1,385 lb

628 kg

Maximum payload (D-E):

5,085 lb

2,307 kg

Fuel with maximum payload (A-D):

16,300 lb

7,394 kg

Performance

Range

Maximum range:

4,010 NM

4,614 SM

7,427 km

(Theoretical range at M 0.74 with 7 passengers/2 crew, NBAA IFR reserves, ISA, typical BOW and maximum allowable fuel. Actual range will be affected by speed, weather, selected options and other factors)

Speed	Mach	kt	mph	km/h
High-speed cruise	0.82	470	541	870
Typical cruise speed	0.80	459	528	850
Long-range cruise speed	0.74	425	489	787

Range Map - Beijing Shanghai Hong Kong

Download Factsheet

Airfield Performance

Takeoff distance:

5,840 ft

1,780 m

(SL, ISA, MTOW)

Landing distance:

2,775 ft

846 m

(SL, ISA, MTOW)

Operating Altitude

Maximum operating altitude:

41,000 ft

12,497 m

Initial cruise altitude:

37,000 ft

11,278 m

Noise Level	Flyover	Approach	Lateral
(EPNdB)	81.2	90.3	86.2

Engines

General Electric CF34-3B turbofans

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

9,220 pounds (41.0 kN) thrust APR

Flat-rating: ISA + 15°C (86°F)

Avionics

Rockwell Collins Pro Line 21 with four 10” x 12” LCD screens and integrated menu control

Dual autopilot with single autothrottle

EFIS/EICAS system with synoptics

Dual FMS-6000 with coupled lateral and vertical nav, performance calculations

Dual Honeywell Laseref V Inertial Reference System with automatic position initialization

Integrated Radio Tuning with Rockwell Collins Pro Line 21 VHF/Nav radios

Integrated electronic standby instruments

Integrated Flight information system

Optional Head-Up Guidance System (HGS) / Bombardier Enhanced Vision System (BEVS)