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| Manufacturer | Canadair |
| Model | CL-2(4) |
| Modification | CL-2 |
| Country | Canada |
| Years | 1946 |
| Type | Passenger aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 35.81 m |
| Length | 28.54 m |
| Height | 8.39 m |
| Wing area | 135.63 m2 |
| Zero fuel weight | - |
| Empty weight | 21243 kg |
| Maximum takeoff weight | 37331 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 4 Rolls-Royce Merlin 626 |
| Power | 4 x 1760 HP |
| Thrust | - |
| Maximum speed | 523 km/h |
| Cruising speed | 465 km/h |
| Rate of climb | - |
| Practical range | 5150 km |
| Service ceiling | 8990 m |
| Hovering ceiling | - |
| Crew | 4-5 |
