| Manufacturer | SOCATA |
| Model | TB-200 Tobago |
| Modification | TB-200 |
| Country | France |
| Years | 1991 |
| 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 | 745 kg |
| Maximum takeoff weight | 1150 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming : IO-360-A1B6 |
| Power | 1 x 200 HP |
| Thrust | - |
| Maximum speed | 265 km/h |
| Cruising speed | 241 km/h |
| Rate of climb | - |
| Practical range | 1179 km |
| Service ceiling | 4877 m |
| Hovering ceiling | - |
| Crew | 1 |
