| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Cessna |
| Model | Cessna 402 Businessliner |
| Country | United States |
| Manufactured from | 1966 year |
| Manufactured to | 1985 year |
| Type | Twin Turboprops |
| Icao | C402 |
| Performance | |
| Engine | 2x Continental TSIO-520-VB |
| Power, hp | 325 hp |
| Power, lbf | Add |
| Avionics | Bendix King Avionics |
| Max cruise speed | 428 km/h |
| Approach speed | 126 km/h |
| Travel range | 2,358 km |
| Fuel economy | Add |
| Service ceiling | 8,199 m |
| Rate of climb | 7.37 m/sec |
| Take off distance | 669 m |
| Landing distance | 757 m |
| Weights | |
| Max take off weight | 3,107 kg |
| Max landing weight | 2,546 kg |
| Max payload | 950 kg |
| Fuel tank capacity | 780 l |
| Baggage volume | 1.9 m³ |
| Dimensions | |
| Seats | 8 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | 1.3 m |
| Cabin width | 1.4 m |
| Cabin length | 3.4 m |
| Exterior length | 11.1 m |
| Tail height | 3.5 m |
| Fuselage diameter | 1.55 m |
| Wing span | 13.5 m |
| Wing tips | No Winglets |