| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Pilatus Aircraft |
| Model | Pilatus PC-7 Mk II |
| Country | Switzerland |
| Manufactured from | 1978 year |
| Manufactured to | Add |
| Type | Military Propellor Planes |
| Icao | Add |
| Performance | |
| Engine | 1 × Pratt & Whitney PT6A-25C |
| Power, hp | 700 hp |
| Power, lbf | Add |
| Avionics | Honeywell Avionics |
| Max cruise speed | 291 km/h |
| Approach speed | Add |
| Travel range | Add |
| Fuel economy | 4.697 km/l |
| Service ceiling | Add |
| Rate of climb | Add |
| Take off distance | 1,180 m |
| Landing distance | 800 m |
| Weights | |
| Max take off weight | 5,952 kg |
| Max landing weight | Add |
| Max payload | 472 kg |
| Fuel tank capacity | Add |
| Baggage volume | 0.03 m³ |
| Dimensions | |
| Seats | 2 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | Add |
| Tail height | Add |
| Fuselage diameter | Add |
| Wing span | Add |
| Wing tips | Add |