Challenger 605 (CL-605) Canadian Transport Aircraft
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Basic Information
Name
Challenger 605 (CL-605) Canadian Transport Aircraft
Designation
—
Alternate Designation
—
Equipment Type
—
Manufacturer
Bombardier Aerospace (1986-present)
Date of Introduction
2006
Description
CL-605 Introduced in early 2006, air frame updated with larger cabin windows and a new tailcone, cockpit updated with the Collins Proline 21 avionics and "electronic flight bag" capability.
Air & Air Defense Specifications
Crew
2
Engine
Turbofan (8730 hp)
Max Speed
1013.6 km/h
Range
7470.0 km
Payload Capacity
2200 kg
System
Alternate Designation(s)
Challenger 605
Primary Function / Type
Transport Aircraft
Manufacturer
Bombardier Aerospace (1986-present)
Crew
2
Passengers
12
Number of Engines
2
Number of Hard Points
INA
Dimensions
Length
20.90 m
Height
6.30 m
Width (Wing Span)
19.60 m
Wing Area
45.4 sq m
Cabin Length
7.80 m
Cabin Width
2.41 m
Cabin Height
1.85 m
Cabin Volume
INA
Maximum Takeoff Weight
21,910 kg
Maximum Landing Weight
17,237 kg
Payload Capacity
2,200 kg
Automotive
Engine Name
2 x GE CF34-3B
Number of Engines
2
Engine Type
Turbofan
Engine Power
8,730 lb (38.8 kN) thrust
High-Speed Cruise Speed
Mach 0.82
Maximum Range
7,470 km
Takeoff Run
1,780 m
Landing Distance
720 m
Protection
Stealth Properties
None
Heat Signature Reduction
No
Add on Armor
INA
NBC Protection
INA
EW Counter Measures
INA
Chaffs/Flares
INA
Details
Country of Origin
Canada
Category
Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
C
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
20.9 m
Width
19.6 m
Height
6.3 m
Weight
21910 kg
Operators (4)
China
Canada
Mexico
United Arab Emirates
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