There are 6 images added between 6 December 2006 and 18 September 2010
Initial Operational Capability (IOC):
Total Production: ?
Also Known As: Mi-34A, Mi-34BPV, Mi-34C1, Mi-34M, Mi-34S, Mi-34S1, Mi-34U, Mi-34UT, Mi-34VA3 and Sapsan
Origin: Russia
Corporations: Mil Helicopter and Progress Arseniev Aircraft Company
Parent System: Mi-34
Initial Operational Capability (IOC):
Total Production: ?
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Description: Mi-34 is a single-engine, light utility helicopter developed by MIL helicopters for both civil and military applications. Despite Mi-34 helicopter production ceased in the late 1990s MIL is studying the chance of re-engining this helicopter with more powerful and reliable engines to re-launch its production. In addition further variants for different purposes might be developed as well.

Mi-34VA3 is a civil variant and Mi-34M is its military counterpart. Mi-34A is a variant powered by France's Arrius or Russian engines (AI-450) rated at approximately 450-shp. Mi-34U features a piston engine with increased power while Mi-34UT is a training variant. Mi-34BPV is a multi-purpose unmanned variant.

Mi-34 Specifications

Crew: 1
Main Rotor Blades: 4
Number of Engines: 1
Passengers: 3
Max Power at TakeOff: 370 shp (276 kW)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Mi-34 News

There is 1 news
on 15 Apr 2011
Friday, April 15, 2011Russian Helicopters Announce New Partnership in Brazil

Operators & Related Equipment


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