Challenger 300

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Overview

Created from a clean sheet, Bombardier Challenger 300 is the definitive, super-midsize corporate jet, developed to satisfy customer needs unmet by any other aircraft

Best performance and value in its class
Incomparable room to conference and work
Supreme reliability, designed for long-term service

Technical Specifications

Capacity

Crew: 2

Typical seating: 8-9 (double-club configuration)

Dimensions

Exterior

Length:

68.7 ft

20.9 m

Wingspan:

63.8 ft

19.5 m

Wing area (basic):

522 ft²

48 m²

Height overall:

20 ft

6.1 m

Interior

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

28.6 ft

8.72 m

Cabin maximum width: (Centerline)

7.2 ft

2.19 m

Cabin width: (Floorline)

5.1 ft

1.55 m

Cabin height:

6.1 ft

1.86 m

Floor area: (Excluding cockpit)

146 ft²

13.56 m²

Cabin volume:
(Excluding cockpit and baggaget)

860 ft³

24.35 m³

Weights

A. Maximum ramp weight:

39,000 lb

17,690 kg

B. Maximum takeoff weight (MTOW):

38,850 lb

17,622 kg

C. Maximum landing weight (MLW):

33,750 lb

15,309 kg

D. Maximum zero fuel weight:

27,000 lb

12,247 kg

E. Typical basic operating weight:

23,700 lb

10,750 kg

F. Maximum fuel weight:

14,150 lb

6,418 kg

Maximum payload (D-E):

3,300 lb

1,497 kg

Payload – full fuel (A-E-F):

1,150 lb

522 kg

Fuel with maximum payload (A-D):

12,000 lb

5,443 kg

Performance

Range

Maximum range:

3,100 NM

3,567 SM

5,741 km

(Theoretical range at M 0.80 with 8 passagers/2 crew, NBAA IFR reserves, ISA, standard 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	458	527	848

Range Map - Beijing Shanghai Hong Kong

Download Factsheet

Airfield Performance

Takeoff distance:

4,810 ft

1,466 m

(SL, ISA, MTOW)

Landing distance:

2,600 ft

792 m

(SL, ISA, MTOW)

Operating Altitude

Maximum operating altitude:

45,000 ft

13,716 m

Initial cruise altitude (MTOW):

41,000 ft

12,497 m

Noise Level(EPNdB)	Flyover (thrust cutback)	Approach	Lateral
	75.5	89.6	87.6

Engines

Honeywell HTF7000 turbofans

Thrust: 6,826 pounds (30.4 kN) at takeoff

9,220 pounds (41.0 kN) thrust APR

Flat-rating: ISA + 15°C (86°F)

Avionics

Rockwell Collins Pro Line 21 with 4 LCD displays

EICAS

Dual FMS 5000, Dual GPS with WAAS, Dual DME

Maintenance diagnostics Computer

EGPWS/TCASII/ELT

IFIS

Cockpit Voice Recorder

Digital Flight Data Recorder