| Manufacturer | SOCATA |
| Model | TB-10 Tobago |
| Modification | TB-10 |
| Country | France |
| Years | 1977 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.04 m |
| Length | 7.75 m |
| Height | 3.02 m |
| Wing area | 12.25 m2 |
| Zero fuel weight | - |
| Empty weight | 700 kg |
| Maximum takeoff weight | 1150 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming O-360-A1AD |
| Power | 1 x 180 HP |
| Thrust | - |
| Maximum speed | 248 km/h |
| Cruising speed | 235 km/h |
| Rate of climb | - |
| Practical range | 1291 km |
| Service ceiling | 3962 m |
| Hovering ceiling | - |
| Crew | 1 |
