Mil Mi-4

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.

Attribution

Attribution

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 devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1-3 in Side-by-side arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

Mikhail Mil. School of the embodiment of ideas
Vertolet
2009 (page 36)
Book

Mil Moscow Helicopter Plant 50 Years
Lyubimaya Kniga
1998 (page 66)
Book

Russian Helicopters, Ka-27
Russian Нelicopters, JSC
5 July 2017 (page 205)
Website

Related VFS Resources

Resources related to the Mi-4 , provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.
Images from the VFS Gallery
Enter a search term in the box above.

Related Public Resources

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

Images