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 |