Attribute | Value |
---|---|
General | |
Manufacturer | MIL Helicopters |
Model | Mil Mi-34 “Hermit” |
Country | Russia |
Manufactured from | 1989 year |
Manufactured to | Add |
Type | Light Helicopters |
Icao | Add |
Performance | |
Engine | 1 × Vedeneev M-14V-26 9-cylinder - |
Power, hp | 320 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 170 km/h |
Approach speed | Add |
Travel range | 450 km |
Fuel economy | 2.945 km/l |
Service ceiling | 4,499 m |
Rate of climb | 9.16 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 1,350 kg |
Max landing weight | Add |
Max payload | 550 kg |
Fuel tank capacity | 174 l |
Baggage volume | 1 m³ |
Dimensions | |
Seats | 3 |
Seats - business class | Add |
Seats - first class | Add |
Cabin height | Add |
Cabin width | Add |
Cabin length | Add |
Exterior length | 11.42 m |
Tail height | Add |
Fuselage diameter | Add |
Wing span | 10.01 m |
Wing tips | No Winglets |