| Manufacturer | Cessna |
| Model | Cessna 401-402 Utiliner |
| Modification | Cessna 402C |
| Country | USA |
| Years | 1966 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 13.45 m |
| Length | 11.09 m |
| Height | 3.49 m |
| Wing area | 21.00 m2 |
| Zero fuel weight | - |
| Empty weight | 1845 kg |
| Maximum takeoff weight | 3107 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 Continental TSIO-520VB |
| Power | 2 x 325 HP |
| Thrust | - |
| Maximum speed | 428 km/h |
| Cruising speed | 394 km/h |
| Rate of climb | - |
| Practical range | 2360 km |
| Service ceiling | 8200 m |
| Hovering ceiling | - |
| Crew | 1-2 |
