Mil Mi-6
Development of the Russian Mi-6 (NATO Designation: 'Hook') heavy transport helicopter began in 1952; production took off in 1957. Under extreme circumstances, the cargo cabin can hold up to 150 people; in the ambulance version, 41 stretchers and 2 seats. Normally, the passenger cabin can accommodate 61 passengers. Maximum internal and slung payloads are 12,000 kg and 8,000 kg, respectively.
Configuration
Primary flight and mechanical characteristicsVTOL type: Compound Helicopter
Compound type: Lift
Lift devices: 1 Single main rotor
Dedicated control device: 1 Tail rotor
Crew required: 5-6 in Side-by-side arrangement
Landing gear: Wheels (non-retractable)
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentRelated VFS Resources
Resources related to the Mi-6 , provided by the Vertical Flight Society.Forum Proceedings
Vertiflite articles
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Related Public Resources
Resources related to the Mi-6 , provided by public sources across the internet.Publicly-funded resources provided by the US Government
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Public resources provided by select scholarly and academic sources
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