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Bombardier Challenger

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Bombardier Challenger

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:

  • CL-600              original production version, powered by Avco Lycoming ALF-502L turbofans of 33.6 kN thrust each.

  • CL-601-1A         refined version including winglets to reduce drag and more powerful General Electric CF34-1A engines.

  • 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.

 

Developing nation: Canada.
Manufacturer/designer:  Bombardier Aerospace.
Production line: Montreal - Dorval IAP, Quebec Canada.
   
Type aircraft: Medium to long range widebody corporate jet.
   
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.

First delivery:  
  Canadair CL-601 Challenger
Cockpit crew: two pilots.
Passengers: up to 19.
Cabin Length: 8,72 m
Cabin diameter: 2,19 m.
Cabin height: 1,85 m.
Cabin floor: 13,56 m².
Cabin Volume: 24,35 m³.
   
Wing span: 19,61 m.
Wing area: 48,31 m².
Wing sweep:  degrees.
Fuselage length: 20,85 m.
Fuselage diameter: 2,49 m.
Height: 6,30 m.
   
Engines:

- two General Electric CF34-1A each rated 40,66 kN.

Weight:

- empty: 9.049 Kg.

- max. zero-fuel weight: 11.151 Kg.

- fuel: 7.559 Kg.

- max. payload: 2.229 Kg.

Max. take off weight: 19.950 Kg.
Max. landing weight: 15.309 Kg.
Cruise speed: 786 km/h.
Max. speed: 851 km/h.
Max. ceiling: 12.495 m.
Range:

- max. range 6.375 km.

Performance:

- 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.

 

 

Canadair Challenger military operators:

Canadian Armed Forces.* 

- 1 CX-144A.

- 2 CC-144.

- 2 CE-144C.

- 2 CU-144A

- 3 CC-144B

- 3 CE-144C

- 4 CC-144A

Luftwaffe (Germany). 

- 6 CL-601-1A

Royal Australian Air Force. 

- 3 CL-604

Royal Danish Air Force. - 3 CL-604
Croatia Government. 

- 1 CL-604

Czech Government. 

- 1 CL-601-3A 

Gouvernement du Quebec. - 1 CL-601
Jordanian Government. - 1 CL-604
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:

 

  • 24apr1995    144613    CC-144B    Canadian Armed Forces    written-off at CFB Shearwater, Canada    0 fatalities / ? on board.

 

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