| Manufacturer | Canadair |
| Model | CL-28 Argus |
| Modification | Argus Mk.I |
| Country | Canada |
| Years | 1957 |
| Type | Search and rescue aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 43.37 m |
| Length | 39.26 m |
| Height | 11.79 m |
| Wing area | 192.77 m2 |
| Zero fuel weight | - |
| Empty weight | 36741 kg |
| Maximum takeoff weight | 71214 kg |
| Normal takeoff weight | 67133 kg |
| Flight duration | 26.30 h |
| Engine | 4 Wright R-3350-TC981-EA1 Turbo-Compound |
| Power | 4 x 3400 HP |
| Thrust | - |
| Maximum speed | 507 km/h |
| Cruising speed | 463 km/h |
| Rate of climb | - |
| Practical range | 9495 km |
| Service ceiling | 7620 m |
| Hovering ceiling | - |
| Crew | 5 + 6 операторов |
