| Manufacturer | Grumman |
| Model | OV-1 Mohawk |
| Modification | OV-1A |
| Country | USA |
| Years | 1959 |
| Type | Attack aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 14.63 m |
| Length | 13.69 m |
| Height | 3.96 m |
| Wing area | 33.45 m2 |
| Zero fuel weight | - |
| Empty weight | 5333 kg |
| Maximum takeoff weight | 8214 kg |
| Normal takeoff weight | 7140 kg |
| Flight duration | 2 h |
| Engine | 2 Textron Lycoming T53-L-701 |
| Power | 2 x 1044 HP |
| Thrust | - |
| Maximum speed | 491 km/h |
| Cruising speed | 428 km/h |
| Rate of climb | - |
| Practical range | 1621 km |
| Service ceiling | 7620 m |
| Hovering ceiling | - |
| Crew | 2 |
