Production of the Mi-4 (NATO Designation: 'Hound') helicopter began in 1952.  The cabin has a capacity to carry up to 16 passengers in addition to up to three crew members.  Maximum internal payload is 1600 kg.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-4

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: 1-3

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 5.18 m (17.0 ft)

Overall Width: 21.00 m (68.9 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 7800 kg (17196 lb)

Max Range: 465 km (251 nm)

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Related Public Resources

Resources related to the Mi-4 , provided by public sources across the internet.

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