| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Cessna |
| Model | Cessna 425 Conquest I |
| Country | United States |
| Manufactured from | 1980 year |
| Manufactured to | 1986 year |
| Type | Twin Turboprops |
| Icao | C425 |
| Performance | |
| Engine | 2x Pratt & Whitney Canada PT6A-112 |
| Power, hp | 450 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 491 km/h |
| Approach speed | 146 km/h |
| Travel range | 3,048 km |
| Fuel economy | Add |
| Service ceiling | 10,577 m |
| Rate of climb | 9.45 m/sec |
| Take off distance | 741 m |
| Landing distance | 654 m |
| Weights | |
| Max take off weight | 3,719 kg |
| Max landing weight | 2,970 kg |
| Max payload | 725 kg |
| Fuel tank capacity | 1,385 l |
| Baggage volume | 1.8 m³ |
| Dimensions | |
| Seats | 8 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | 1.3 m |
| Cabin width | 1.4 m |
| Cabin length | 3.2 m |
| Exterior length | 10.9 m |
| Tail height | 3.8 m |
| Fuselage diameter | 1.55 m |
| Wing span | 13.4 m |
| Wing tips | No Winglets |