Attribute | Value |
---|---|
General | |
Manufacturer | MIL Helicopters |
Model | MIL Mi-26 |
Country | Russia |
Manufactured from | 1981 year |
Manufactured to | Add |
Type | Large Helicopters |
Icao | MI26 |
Performance | |
Engine | 2x 2 × Lotarev D-136 turboshafts |
Power, hp | 11,400 hp |
Power, lbf | Add |
Avionics | Groza 7A813 weather radar, Integrated PKV-26-1 flight/nav system |
Max cruise speed | 294 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 | 9 |
Seats - first class | 65 |
Cabin height | 3.2 m |
Cabin width | 3.1 m |
Cabin length | 12.1 m |
Exterior length | 40.03 m |
Tail height | 7.95 m |
Fuselage diameter | Add |
Wing span | 32 m |
Wing tips | No Winglets |