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Mil Mi-6

Mil Mi-6A, Aeroflot, RA-21133, c/n 715309, Museum Hermeskeil © Karsten Palt
Photo ©: Karsten Palt

Mi-6

Heavy Transport Helicopter

Crew5
Passengers65
 
Propulsion2 Turboshaft Engines
Engine ModelSolowjew / Soloviev D-25V
Engine Power (each)4045 kW5424 shp
 
Speed300 km/h162 kts
  186 mph
Service Ceiling4.500 m14.764 ft
Range620 km335 NM
386 mi.
 
Empty Weight27.240 kg60.054 lbs
max. Takeoff Weight42.500 kg93.696 lbs
 
Rotor Blades (main/tail)5/45/4
Main Rotor Diameter35,00 m114,8 ft
Tail Rotor Diameter6,30 m20,7 ft
Rotor Disc Area962,1 m²10356 ft²
Length41,74 m136,9 ft
Height9,86 m32,3 ft
 
First Flight05.06.1957
Production Statusout of production
Total Production>800
 
NATO CodeHook
Data for (Version)Mil Mi-6A

WeblinksExtras
MIL Moscow helicopter plant, JSC

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