Attribute | Value |
---|---|
General | |
Manufacturer | MIL Helicopters |
Model | Mil Mi-26 “Halo” |
Country | Russia |
Manufactured from | 1986 year |
Manufactured to | Add |
Type | Military Helicopters |
Icao | Add |
Performance | |
Engine | 2 × Lotarev D-136 turboshafts - |
Power, hp | 11,240 hp |
Power, lbf | Add |
Avionics | Add |
Max cruise speed | 256 km/h |
Approach speed | Add |
Travel range | 1,952 km |
Fuel economy | 0.186 km/l |
Service ceiling | 4,602 m |
Rate of climb | 7.73 m/sec |
Take off distance | Add |
Landing distance | Add |
Weights | |
Max take off weight | 56,000 kg |
Max landing weight | Add |
Max payload | 20,000 kg |
Fuel tank capacity | 12,000 l |
Baggage volume | 6.16 m³ |
Dimensions | |
Seats | 9 |
Seats - business class | 65 |
Seats - first class | Add |
Cabin height | 3.2 m |
Cabin width | 3.1 m |
Cabin length | 12.1 m |
Exterior length | 40.03 m |
Tail height | Add |
Fuselage diameter | Add |
Wing span | 32 m |
Wing tips | No Winglets |