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 |