| Manufacturer | SOCATA |
| Model | ST-10 Diplomate |
| Modification | ST-10 |
| Country | France |
| Years | 1966 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.70 m |
| Length | 7.26 m |
| Height | 2.88 m |
| Wing area | 13.00 m2 |
| Zero fuel weight | - |
| Empty weight | 723 kg |
| Maximum takeoff weight | 1220 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming IO-360-C1B |
| Power | 1 x 200 HP |
| Thrust | - |
| Maximum speed | 280 km/h |
| Cruising speed | 265 km/h |
| Rate of climb | - |
| Practical range | 1385 km |
| Service ceiling | 5000 m |
| Hovering ceiling | - |
| Crew | 1 |
