1983 - 1987 Challenger CL601-1A

The 601-1A received its Supplemental Type Certificate (STC for the 1A) in 1983. It was in production from 1983 to 1987 and 66 were produced. It is essentially a model 600 with General Electric CF-34-1A engines. When the engines go through hot-section or overhaul they may be upgraded to the 601-3A performance. More than half the fleet has taken advantage of this option. The range of the 601-1A with seats full is 3,180 nm with NBAA IFR reserves.
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Aircraft Information
Year: 1983 - 1987
Make: Challenger
Model: CL-601-1A
Active Fleet: 59  -  For Sale/Lease: 5
Average Asking Price - February 2014: $1,748,000
Range: 3,180 - 3,450 nm
Contact Number: 1-847-726-5000
Current Market Price / Availability: REQUEST MARKET UPDATE REPORT
General Performance & Specifications
Cabin Height: 6.1 Feet
Cabin Width: 8.2 Feet
Cabin Length: 28.30 Feet
Baggage Volume Internal: 115.0 Cubic Feet
Seats Executive: *2/9
Max. Take-Off Weight: 43,100 lbs.
Max. Landing Weight: 36,000 lbs.
Maximum Payload: 3,600 lbs.
Balance Field Length: 6,300 Feet
Landing Distance: 4,700 Feet
Rate of Climb - All Engines: 4,200 Feet / Minute
Rate of Climb - One Engine Out: 1,048 Feet / Minute
Normal Cruise Speed: 443 ktas
Max. Cruise Speed: 459 ktas
Service Ceiling Max. Weight: 39,000 Feet
Number of Engines: 2
Engine Manufacturer: GE
Engine Model: CF34-1A
Description

The 601-1A received its Supplemental Type Certificate (STC for the 1A) in 1983. It was in production from 1983 to 1987 and 66 were produced. It is essentially a model 600 with General Electric CF-34-1A engines. When the engines go through hot-section or overhaul they may be upgraded to the 601-3A performance. More than half the fleet has taken advantage of this option. The range of the 601-1A with seats full is 3,180 nm with NBAA IFR reserves.