Aircraft - Challenger CL 604

Long range wide body corporate jets
GENERAL INFORMATION
The Challenger 601 concentrated on the original CL-600 Challenger's weight problems and replaced the troubled ALF-502 turbofans, creating a highly unbeaten full size corporate jet.Troubles with the Avco Lycoming powered Challenger 600 led Canadair (now a part of Bombardier) to develop a vastly improved variant in the form of the General Electric CF-34 powered Challenger 601. Another important change was the addition of winglets, which are also offered as a retrofit to earlier aircraft. The 601 first flew on April 10 1982. The 600 was dropped from the model line in 1983.
Subsequent development of the Challenger led to the 601-3A. First flying in 1987, this variant introduced an EFIS glass flight deck and upgraded engines. Available from 1989, the 601-3R was an extended range model with higher weights (the range increase modifications can also be retrofitted to earlier 601-3As).

PERFORMANCE
604 - Max cruising speed 882km/h (476kt), normal cruising speed 851km/h (459kt), long range cruising speed 787km/h (425kt). Certified ceiling 41,000ft. Range with max fuel, five pax and reserves 7550km (4077nm) at long range cruising speed, 6980km (3769nm) at normal cruising speed.
CAPACITY
Flight crew of two. Various seating options available depending on customer preference, maximum permissible seating for 19. Generally the aircraft is used as a Business Jet with a executive seating configuration of 09 to 12 seats.