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Canadair CL-600 Challenger


The CL-600 Challenger was designed by Bill Lear and was originally designated Learstar 600. Canadair bought the rights to the design in 1976 and further developed it to feature a large fuselage cross section which allows for 6’1"(1.85m) headroom. Production of the CL-600 ceased in 1983 so that the company could concentrate on the upgraded CL-601 model. 76 of the original CL-600’s have been retro-fitted with winglets and have the designation CL-600S.

Canadair CL-600 Challenger

N100LR                    c/n 1064                  Canada

21 seat executive jet first flown in 1978

Engines: 2x 7500lb.s.t.(33.3kN) Lycoming ALF502L                                                                        Length: 68’5"(20.85m)                                                                                          Height: 20’8"(6.3m)Wingspan: 61’10"(18.85m)                                                                                               No.built: 84 Range: 3220miles(5182km)                                                           Cruising speed: 505mph(812kmh) Empty weight: 18,660lb(8471kg)                                      Maximum take-off weight: 41,100lb(18,659kg)

Another example of the CL-600 is illustrated below.

  Canadair CL-600 Challenger

                                       OE-HET                    c/n 1085

 

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