Mil Mi-4

General Data
First Flown:	1952	Length:	16.8 m
Lift Capability:	5.6 m	Height:
Range:		Rotor Span:	21 m
Top Speed:	99 mph	Empty Weight:
Service Ceiling:		Max Gross Weight:	17,200 lbs
Engines:	1 1,700 shp Shvetson ASh-82V, air-cooled radial piston engine
Armament:	Machine gun pod, rockets
Accommodations:	2 crew and up to 14 fully loaded troops	Cargo:	1,600 kg
Operators:	Afghanistan, Albania, Algeria, Bulgaria, Cuba, Czech Republic, Egypt, Germany, Iraq, Mali, Mongolia, North Korea, North Yemen, People’s Republic of China , Poland, Romania, Somalia , South Yemen, Sudan, Syria, Vietnam

Similar Aircraft:	Sikorsky S-55
Other Features:	clam shell rear doors


Notes
Approx 3,000 were built with production ending in 1969.
NATO designation HOUND

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