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
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
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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