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Mitsubishi MH-2000

Lighter-Than-Air Craft and Rotorcraft

The Mitsubishi MH2000 was a seven to twelve seat light utility helicopter and Japan's first indigenous helicopter, developed and built by Mitsubishi Heavy Industries, which was solely responsible for both the fuselage and the engines. The programme launched in April 1995 for passenger and business transport, law enforcement, search and rescue and air ambulance work. Its engine module and dynamic system sit behind the cabin to keep the passenger compartment quiet, and a pair of Mitsubishi turboshaft engines power it. The first of four development aircraft flew on 29 July 1996 and the first production aircraft was delivered in 2000. A tail rotor failure suspended the type certificate, and Mitsubishi halted marketing and production in September 2004.

Facts
Year
1996 1
Engine Class
Turboshaft 1
Status
Out of production 1
Power (kW)
597 1
Mass (kg)
2500 1
Maximum Mass (kg)
4500 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Mitsubishi MH-2000 (Wikipedia)

Of Make

Source Mitsubishi MH-2000 (Wikipedia)
Sources
1. Mitsubishi MH-2000 (Wikipedia)
  • Lead
    is a 7/12 seat light utility helicopter
  • Lead, first flight
    first flew on 29 July 1996
  • Lead, production
    Mitsubishi ultimately decided to halt marketing and production of the MH2000 in September 2004
  • Specifications, empty weight
    Empty weight: 2,500 kg (5,512 lb)
  • Specifications, max takeoff weight
    Max takeoff weight: 4,500 kg (9,921 lb)
  • Specifications, powerplant
    597 kW (801 hp) each
  • Lead, engine
    Power was provided by a pair of Mitsubishi MG5-100 turboshaft engines
  • Lead, manufacturer
    was primarily developed and produced by Mitsubishi Heavy Industries (MHI)
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