| Manufacturer | Grob |
| Model | G.115TA |
| Modification | G.115TA |
| Country | Germany |
| Years | 1992 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10,00 m |
| Length | 8,20 m |
| Height | 2,57 m |
| Wing area | 12.21 m2 |
| Zero fuel weight | - |
| Empty weight | 900 kg |
| Maximum takeoff weight | 1350 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 x Textron Lycoming AEIO-540-D4A5 |
| Power | 1 x 194 HP |
| Thrust | - |
| Maximum speed | 426 km/h |
| Cruising speed | 306 km/h |
| Rate of climb | - |
| Practical range | 1310 km |
| Service ceiling | 5485 m |
| Hovering ceiling | - |
| Crew | 2 |
