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Mitsubishi MH2000

1996

After obtaining big experience building models under license, Mitsubishi Heavy Industries began development of first indigenous helicopter manufacturing both the fuselage and engines. An experimental aircraft, the Mitsubishi RP-1, used a conventional tail rotor and first flew on September 14, 1994. In 1995 began development of the MH2000, a 7/12 seats helicopter fitted with a Fenestron-like tail rotor, which completed maiden flight on July 29, 1996 and achieving Japanese certification on August 1997. The prototype was lost due to tail rotor blade separation and after redesign the production aircraft were known as MH2000A. The type entered service October 1, 2000 with Excel air service but program was terminated in 2004 with only 8 aircraft built.

Specifications

Engine2 x Mitsubishi MG5-110 800 shp
Capacity2 + 10
Length (m)12.2
Height (m)4.1
Blades4
Rotor diam. (m)12.2
Disc area (m2)117
Weight (kgs)Empty: 2500 Max: 4500
Speed (km/h)Cruise: 250 Max: 278
Range (km)777
blueprints MH2000

Airframes (8)

C/NModelBuiltReg
1001mh20001996JP JQ6003
1002mh20001998JP JA001M
1003mh20001999JP JA002M
1004mh20001999JP JA21ME JA21ME
1005mh2000JP JA003M
1006mh2000JP JQ6006
1007mh2000JP JQ6007
1008mh2000JP JA007E