Mil Mi-6A
An updated version of the Mil Mi-6. The capacity of the helicopter is increased, allowing between 65 and 90 passengers, normally. Maximum internal and slung payloads are 12000 kg and 9000 kg, respectively; the 9 tonne payload allows the aircraft to replace cranes for heavy cargo transport.
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 5-6
Crew seating: Other
Landing gear: Wheels (non-retractable)
Overall Dimensions
Data on aircraft sizeOverall Width: 35.00 m (114.8 ft)
Engine Details
Aircraft powerplant (lift and/or propulsion)Total number of engines: 2
Engine designation: Soloviev D-25V turbine
Engine manufacturer: Soloviev Design Bureau
Take-off / rated power: 4103 kW (5500 hp)
Weights and Performance
Data on aircraft weight and flight characteristicsMax Gross Weight (ground): 44000 kg (97003 lb)
Max Range: 620 km (335 nm)
