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The Bombardier
(Canadair) CL-600 Challenger, a medium to long
range widebody corporate jet, was developed by
Learjet designer Bill Lear. Known as the
LearStar 600, this design was first conceived in
1974. In 1976 Canadair purchased the exclusive
production, development and marketing rights.
Three
development Challengers were built, the first of
which flew for the first time on November 8
1978, the others flying in March and July the
following year. However the first aircraft
crashed in a deep stall accident and while
certification was granted in August 1980.
Bombardier
Challenger types:
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CL-600 original production
version, powered by Avco Lycoming ALF-502L
turbofans of 33.6 kN thrust each.
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CL-601-1A refined version including
winglets to reduce drag and more powerful
General Electric CF34-1A
engines.
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CL-601-3A further up-rated engine
and a glass cockpit. This was the first
version marketed by Bombardier.
-
CL-604 major upgrade of the 601
design, incorporating more powerful General
Electric CF34-3B engines, larger fuel
supply, completely new undercarriage,
structural improvements to wings and tail,
and a new electronic flight instrumentation
system.
-
Challenger
300 a new-generation CL-604 with two
Honeywell AS907 turbofan engines each
providing 35.81 kN thrust.
-
Challenger
800 a variant of the Bombardier Regional
Jet airliner, has a 5.778 km
transcontinental range.
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Developing nation: |
Canada. |
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Manufacturer/designer: |
Bombardier Aerospace. |
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Production line: |
Montreal - Dorval IAP, Quebec Canada. |
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Type aircraft: |
Medium to long range widebody corporate jet. |
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First flights: |
- CL-600 November 8, 1978 C-GCGR-X.
- CL-601-1A September 17,
1982.
- CL-601-3A September 28,
1986.
- CL-604 March 17,1995 C-FVUC.
- Challenger 300 August 14,
2001 C-GJCJ.
- Challenger 800 October
13,1996 C-FBGX. |
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First delivery: |
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Canadair CL-601 Challenger |
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Cockpit crew: |
two pilots. |
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Passengers: |
up to 19. |
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Cabin Length: |
8,72 m |
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Cabin diameter: |
2,19 m. |
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Cabin height: |
1,85 m. |
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Cabin floor: |
13,56 m². |
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Cabin Volume: |
24,35 m³. |
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Wing span: |
19,61 m. |
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Wing area: |
48,31 m². |
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Wing sweep: |
degrees. |
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Fuselage length: |
20,85 m. |
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Fuselage diameter: |
2,49 m. |
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Height: |
6,30 m. |
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Engines: |
- two General Electric
CF34-1A each rated 40,66 kN. |
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Weight: |
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empty: 9.049 Kg.
- max. zero-fuel weight:
11.151 Kg.
- fuel: 7.559 Kg.
- max. payload: 2.229 Kg. |
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Max. take off weight: |
19.950 Kg. |
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Max. landing weight: |
15.309 Kg. |
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Cruise speed: |
786 km/h. |
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Max. speed: |
851 km/h. |
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Max. ceiling: |
12.495 m. |
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Range: |
- max.
range 6.375 km. |
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Performance: |
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max. rate of climb at sea level 1.355 m per minute.
- take-off run 1.646 m at
max. take-off weight.
- landing run 1.082 m at max.
landing weight. |
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Canadair
Challenger military operators: |
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Canadian Armed
Forces.* |
- 1
CX-144A.
- 2 CC-144.
- 2
CE-144C.
- 2 CU-144A
- 3 CC-144B
- 3 CE-144C
- 4 CC-144A |
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Luftwaffe
(Germany). |
- 6
CL-601-1A |
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Royal Australian
Air Force. |
- 3 CL-604
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Royal Danish Air
Force. |
- 3 CL-604 |
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Croatia
Government. |
- 1 CL-604 |
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Czech
Government. |
- 1 CL-601-3A |
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Gouvernement du
Quebec. |
- 1 CL-601 |
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Jordanian
Government. |
- 1 CL-604 |
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Korea Maritime. |
- 1 CL-604 |
Summary
May 2005.
*
delivered original
as
1 CX-144A test
aircraft by AETE, Cold Lake
4 CC-144B VIP and
utility transports
7 CE-144A electronic
warfare trainers
3 CP-144A maritime
patrol aircraft
2 CC-144 VIP utility
transport |
1 military Bombardier Challengers written-off by
accidents:
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Posters







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