| Manufacturer | Canadair |
| Model | CL-601 Challenger |
| Modification | CL-601 |
| Country | Canada |
| Years | 1982 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 19.61 m |
| Length | 20.85 m |
| Height | 6.30 m |
| Wing area | 48.31 m2 |
| Zero fuel weight | - |
| Empty weight | 9049 kg |
| Maximum takeoff weight | 19550 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 General Electric CF34-1A |
| Power | - |
| Thrust | 2 x 38.48 (40.66) kN |
| Maximum speed | - |
| Cruising speed | 851 km/h |
| Rate of climb | - |
| Practical range | 6371 km |
| Service ceiling | 12495 m |
| Hovering ceiling | - |
| Crew | 2 |
