Canadair CL-600 Challenger specs
| Manufacturer: | Canadair |
| Country: |  Canada |
| ICAO Type designator: | CL60 |
| First flight: | 8 November 1978 |
| Production ended: | in production |
| Production total: | 796+ |
| Series: | CC-144A Challenger: Designation for Royal Canadian Air Force
CL-600-1A11 Challenger 600: Original production version CL-600-2A12 Challenger 601: Version including winglets and GE CF34-1A engines CL-600-2B16 Challenger 601-3A: GE CF34-3A engines with a higher flat rating and a glass cockpit. CL-600-2B16 Challenger 601-3R: Standard tail tank and CF34-3A1 Engines CL-600-2B16 Challenger 604: GE CF34-3B engines; increased fuel capacity, structural improvements to wings and tail; new avionics |
| Propulsion: | 2 jet engines |
| Maximum number of passengers: | 11 |
| Maximum take-off mass: | 18201 kg |
| ICAO Mass group: | 3 |
Canadair CL-600 Challenger file photo (photo: Aviation Safety Network archives)
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