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.
Aircraft Information
General Performance & Specifications
Description
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 |
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.
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