| Manufacturer | SOCATA |
| Model | TBM-700 |
| Modification | TBM-700 |
| Country | France |
| Years | 1988 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.68 m |
| Length | 10.64 m |
| Height | 4.35 m |
| Wing area | 18.00 m2 |
| Zero fuel weight | - |
| Empty weight | 1860 kg |
| Maximum takeoff weight | 2984 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Pratt Whitney Canada PT6A-64 |
| Power | 1 x 1580 HP |
| Thrust | - |
| Maximum speed | 365 km/h |
| Cruising speed | 345 km/h |
| Rate of climb | - |
| Practical range | 2870 km |
| Service ceiling | 9140 m |
| Hovering ceiling | - |
| Crew | 1-2 |
