| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Mitsubishi Heavy Industries |
| Model | Mitsubishi MU-2 |
| Country | Japan |
| Manufactured from | 1963 year |
| Manufactured to | 1986 year |
| Type | Twin Turboprops |
| Icao | MU2 |
| Performance | |
| Engine | 2x Honeywell TPE331-6-251M |
| Power, hp | 776 hp |
| Power, lbf | Add |
| Avionics | Add |
| Max cruise speed | 546 km/h |
| Approach speed | 150 km/h |
| Travel range | 2,334 km |
| Fuel economy | Add |
| Service ceiling | 9,019 m |
| Rate of climb | 11.99 m/sec |
| Take off distance | 661 m |
| Landing distance | 573 m |
| Weights | |
| Max take off weight | 5,250 kg |
| Max landing weight | 5,000 kg |
| Max payload | 1,726 kg |
| Fuel tank capacity | 1,389 l |
| Baggage volume | 1.2 m³ |
| Dimensions | |
| Seats | 12 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | 1.32 m |
| Cabin width | 1.5 m |
| Cabin length | 4.87 m |
| Exterior length | 12.01 m |
| Tail height | 4.17 m |
| Fuselage diameter | 1.6 m |
| Wing span | 12.01 m |
| Wing tips | No Winglets |