| Manufacturer | SOCATA |
| Model | TB-21 Trinidad |
| Modification | TB-21 |
| Country | France |
| Years | 1984 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.97 m |
| Length | 7.75 m |
| Height | 2.85 m |
| Wing area | 11.90 m2 |
| Zero fuel weight | - |
| Empty weight | 867 kg |
| Maximum takeoff weight | 1400 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming TIO-540-AB1AD |
| Power | 1 x 250 HP |
| Thrust | - |
| Maximum speed | 365 km/h |
| Cruising speed | 351 km/h |
| Rate of climb | - |
| Practical range | 1917 km |
| Service ceiling | 7620 m |
| Hovering ceiling | - |
| Crew | 1 |
