| Attribute | Value |
| General |
| Manufacturer | North American Aviation NAA |
| Model | North American Rockwell OV-10 Bronco |
| Country | United States |
| Manufactured from | 1965 year |
| Manufactured to | 1986 year |
| Type | Military Propellor Planes |
| Icao | V10 |
| Performance |
| Engine | 2x Garrett T76-G-420/421 |
| Power, hp | 1,040 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 463 km/h |
| Approach speed | 83 km/h |
| Travel range | 2,222 km |
| Fuel economy | Add |
| Service ceiling | 7,925 m |
| Rate of climb | 13.46 m/sec |
| Take off distance | 853 m |
| Landing distance | 381 m |
| Weights |
| Max take off weight | 6,552 kg |
| Max landing weight | Add |
| Max payload | 1,679 kg |
| Fuel tank capacity | 954 l |
| Baggage volume | 3.1 m³ |
| Dimensions |
| Seats | 2 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 13.41 m |
| Tail height | 4.6 m |
| Fuselage diameter | 1.2 m |
| Wing span | 12.2 m |
| Wing tips | No Winglets |