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Mitsubishi MU-2B-60

The MU-2B-60 is the MU-2 approved by the FAA in March 1978 for 8 to 11 people. Two Honeywell, formerly Garrett and AiResearch, TPE331-10-501M or TPE331-10-511M turboprops of 715 shaft horsepower turn propellers 98 inches across. The FAA data sheet gives a maximum takeoff weight of 11,575 lb, or 5,250 kg, up to 11 seats including the pilot, and 364 or 403 US gallons of usable fuel, depending on which outer tanks are fitted. It files under the ICAO code MU2, as every MU-2 does. No source read gives its dimensions or its ceiling, so this page has no drawing.

Engines
Two Honeywell TPE331-10-501M or TPE331-10-511M turboprops on the wings
Max takeoff weight
11,600 lb (5,250 kg)

Photos from members

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Specifications

StatusStill flying with a few operators
Type codesICAO MU2

Private aircraft show specs and photos.

Sources