The Mitsubishi MU-2 is a Japanese high-wing, twin-engine turboprop aircraft with a pressurised cabin, built by Mitsubishi Heavy Industries and the company's first postwar aircraft design. Work began in 1959 on a light twin turboprop transport for civil and military roles, and the first MU-2 flew on 14 September 1963. Over-wing spoilers replace ailerons for roll control, which allows very large full-span flaps and gives a high cruise speed with a low landing speed. Aircraft were built in Japan and, from 1965, assembled at San Angelo, Texas, and 704 were made before production ended in 1986. It is one of postwar Japan's most successful aircraft, and Japanese ground forces flew it as the LR-1.
Facts
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Mitsubishi MU-2 (Wikipedia)
Of Make
Source Mitsubishi MU-2 (Wikipedia)
Sources
1. Mitsubishi MU-2 (Wikipedia)
Lead
is a Japanese high-wing, twin-engined, turboprop aircraft with a pressurized cabin manufactured by Mitsubishi Heavy Industries
Lead, first flight
It made its maiden flight in September 1963
Lead, production
was produced until 1986
Lead, production, units built
with 704 manufactured in Japan and San Angelo, Texas, in the United States
Specifications, empty weight
Empty weight: 3,433 kg (7,568 lb)
Specifications, max takeoff weight
Max takeoff weight: 5,250 kg (11,574 lb)
Specifications, powerplant
turboprop engines, 579 kW (776 hp) each
Specifications, powerplant, engine class
2 × AiResearch TPE331-6-251M turboprop engines
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