| Manufacturer | Cessna |
| Model | Cessna 310 |
| Modification | Cessna 310R |
| Country | USA |
| Years | 1953 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.25 m |
| Length | 9.74 m |
| Height | 3.25 m |
| Wing area | 16.60 m2 |
| Zero fuel weight | - |
| Empty weight | 1480 kg |
| Maximum takeoff weight | 2495 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Continental IO-520MB |
| Power | 1 x 285 HP |
| Thrust | - |
| Maximum speed | 383 km/h |
| Cruising speed | 360 km/h |
| Rate of climb | - |
| Practical range | 2840 km |
| Service ceiling | 6020 m |
| Hovering ceiling | - |
| Crew | 1 |
