| Manufacturer | Grumman |
| Model | G-22 Gulfhawk |
| Modification | G-22 |
| Country | USA |
| Years | 1936 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.69 m |
| Length | 7.05 m |
| Height | 3.28 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | - |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Wright GR-1820-G1 |
| Power | 1 x 1000 HP |
| Thrust | - |
| Maximum speed | 467 km/h |
| Cruising speed | 354 km/h |
| Rate of climb | - |
| Practical range | 1609 km |
| Service ceiling | 9755 m |
| Hovering ceiling | - |
| Crew | 1 |
