| Manufacturer | Canadair |
| Model | CL-215 |
| Modification | CL-215 |
| Country | Canada |
| Years | 1967 |
| Type | Search and rescue aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 28.60 m |
| Length | 19.82 m |
| Height | 8.98 m |
| Wing area | 100.33 m2 |
| Zero fuel weight | - |
| Empty weight | 12220 kg |
| Maximum takeoff weight | 19731 kg |
| Normal takeoff weight | 17100 kg |
| Flight duration | - |
| Engine | 2 Pratt Whitney R-2800-CA3 Double Wasp |
| Power | 2 x 2100 HP |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 291 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 6020 m |
| Hovering ceiling | - |
| Crew | 2 |
