Mitsubishi MU-2

Mitsubishi Aircraft International · Japan · first flew 1963 · light aircraft

The Mitsubishi MU-2 is a Japanese high-performance twin-turboprop utility and business aircraft with an unconventional high-lift wing system, widely operated in civilian and military roles since 1965.

Recognition (WEFT)

W — WingsHigh-mounted, straight
E — Engines2 × turboprop, wing-mounted
F — FuselageStubby fuselage with large oval cabin windows and T-tail empennage
T — TailT-tail

WEFT is AircraftIQ's four-point recognition method — how it works.

Spot it by:

Distinctive high-wing twin turboprop with no visible ailerons on the straight wing (replaced by spoilers), prominent fuselage sponsons for the main undercarriage, and a T-tail; short stubby fuselage relative to wingspan.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

Mitsubishi began MU-2 development in the late 1950s as an executive transport; it first flew on 14 September 1963 and entered production both in Japan and at a US facility in San Angelo, Texas, for the North American market. The type uses full-span double-slotted flaps and spoilers instead of ailerons to achieve excellent short-field performance from a high-speed wing. Over 700 were built by the end of production in 1986.

Variants

Numerous variants from the short-fuselage MU-2B through the stretched MU-2L (Marquise) and MU-2N (Solitaire); military versions designated LR-1 and MU-2S served with the JGSDF and JASDF for liaison and search-and-rescue.

Where you'll see it

Widely operated globally in corporate, charter, and utility roles; military versions served the JGSDF and JASDF into the 2000s. A contentious safety record in the US led to FAA-mandated special pilot training requirements from 2008.

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