| 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 |