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.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-6

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL 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 size

Overall 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 characteristics

Max Gross Weight (ground): 44000 kg (97003 lb)

Max Range: 620 km (335 nm)

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