| Primary Function: | Heavy cargo-transport | | Contractor: | Mil | | Crew: | Four - two pilots, flight engineer and navigator, and loadmaster | | Unit Cost: | N/A | | Powerplant | | | Two 10,000shp (7460kW) ZMKB Progress D-136 turboshafts driving an eight blade main rotor and five blade tail rotor | | Dimensions | | Fuselage Length: | 110 ft, 8 in (33.73 m) | | Rotor Diameter: | 105 ft (32 m) | | Height: | 26 ft, 9 in (8.15 m) | | Weights | | Empty: | 62,170lb (28,200kg) | | Maximum Takeoff: | 123,450lb (56,000kg) | | Performance | | Speed: | 160kt (295km/h / 184.8 mph) | | Ceiling: | 15,100ft | | Range: | 1036nm (1920km) -- (w/ four aux. fuel tanks) | | Armament | | | N/A | |
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