Neha Patil (Editor)

Mil Mi 34

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Top speed
  
210 km/h

Length
  
11 m

Wingspan
  
10 m

First flight
  
November 17, 1986

Mil Mi-34 Mil Mi34 pictures technical data history Barrie Aircraft Museum

Manufacturer
  
Mil Moscow Helicopter Plant

The Mil Mi-34 (NATO reporting name: Hermit) is a light helicopter designed by the Mil Moscow Helicopter Plant in either a two or four seat configuration for utility and training. It was first flown on 17 November 1986 and introduced at the Paris Air Show in 1987. The Mi-34 entered production in 1993, and is capable of performing aerobatic maneuvers, including rolls and loops.

Contents

Mil Mi-34 Mil Mi34 Wikipedia la enciclopedia libre

Variants

Mil Mi-34 Mil Mi34 Moscow Police Aviation Photo 2097531 Airlinersnet

  • Mi-34S - four seat production model powered by a 239 kW (325 hp) Vedeneyev (VOKBM) M-14V-26V nine-cylinder, air-cooled, radial engine mounted sideways in the fuselage, and equipped with modern avionics. A few aircraft were purchased by the Moscow police.
  • Mi-34S2 "Sapsan" - turbine version of the Mi-34. It will be able to accommodate up to 4 passengers and the first deliveries are planned by the end of 2011. It will be powered by Turbomeca Arrius-2F
  • Mi-34L - proposed version powered by a 261 kW (350 hp) Textron Lycoming TIO-540J piston engine. None built.
  • Mi-34P Patrulnyi (English: patrol) - Police patrol version for Moscow Mayor Office.
  • Mi-34A - Luxury version, intended to be powered by an Allison 250-C20R turboshaft engine. None built.
  • Mi-34M1 and Mi-34M2 - Proposed twin-turbine, six-passenger versions.
  • Mi-34UT - trainer with dual control.
  • Mi-34V or Mi-34VAZ or Mi-234 - proposed version powered by two VAZ-4265 rotary piston engines.
  • Mi-44 - proposed development with TV-O-100 engine and refined aerodynamics. A mockup was built in 1987.

    • Military operators

     Bosnia and Herzegovina
  • Armed Forces of Bosnia and Herzegovina
    •  Nigeria
  • Nigerian Air Force

    • Specifications (Mil Mi-34)

    Data from Jane's All The World's Aircraft 2003–2004

    General characteristics

    Mil Mi-34 Mil Mi34S Untitled Aviation Photo 1599228 Airlinersnet

  • Crew: 1 or 2 pilots
  • Capacity: 2 passengers
  • Length: 11.415 m (37 ft 5½ in)
  • Rotor diameter: 10.00 m (32 ft 9¾ in)
  • Height: 2.75 m (9 ft 0¼ in)
  • Disc area: 78.70 m² (847.1 ft²)
  • Empty weight: 950 kg (2,094 lb)
  • Max. takeoff weight: 1,450 kg (3,196 lb)
  • Powerplant: 1 × Vedeneyev M-14V-26V nine-cylinder air-cooled radial engine, 239 kW (320 hp)

    • Performance

    Mil Mi-34 Mil Mi34 Moscow Police Aviation Photo 2097531 Airlinersnet

  • Maximum speed: 210 km/h (113 knots, 130 mph)
  • Cruise speed: 170 km/h (92 knots, 106 mph)
  • Range: 356 km (192 nmi, 221 miles)
  • Service ceiling: 4,000 m (13,120 ft)

    • Mil Mi-34 barrieaircraftcomimagesmilmi3402jpg

    Mil Mi-34 Mil Mi34 helicopter development history photos technical data

    References

    Mil Mi-34 Wikipedia
    (Text) CC BY-SA