Attribute | Value |
---|---|
General | |
Manufacturer | Piper Aircraft |
Model | Piper PA-42 Cheyenne III |
Country | United States |
Manufactured from | 1979 year |
Manufactured to | 1993 year |
Type | Twin Turboprops |
Icao | PA42 |
Performance | |
Engine | 2x P&WC PT6A-41/61 |
Power, hp | 720 hp |
Power, lbf | Add |
Avionics | Collins FCB 65 five-tube EFIS, Collins FCB 65 flight director, and APS 65 autopilot etc. |
Max cruise speed | 565 km/h |
Approach speed | 143 km/h |
Travel range | 4,204 km |
Fuel economy | Add |
Service ceiling | 10,668 m |
Rate of climb | 11.35 m/sec |
Take off distance | 985 m |
Landing distance | 920 m |
Weights | |
Max take off weight | 5,080 kg |
Max landing weight | 4,685 kg |
Max payload | 1,890 kg |
Fuel tank capacity | 2,127 l |
Baggage volume | 0.87 m³ |
Dimensions | |
Seats | 1 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | 1.35 m |
Cabin width | 1.3 m |
Cabin length | 5.5 m |
Exterior length | 13.2 m |
Tail height | 4.5 m |
Fuselage diameter | 1.38 m |
Wing span | 14.5 m |
Wing tips | No Winglets |