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Mitsubishi MU-2

ICAO aircraft code MU2
Country Japan

The Mitsubishi MU-2 is a Japanese high-wing, twin-engine turboprop aircraft with a pressurized cabin manufactured by Mitsubishi Heavy Industries.

Specifications

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Mitsubishi MU-2 Specifications

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General

ICAO aircraft code
MU2
Manufacturer
Mitsubishi Heavy Industries
Manufactured
1963 - 1986
Country
Japan

Aircraft performance

Engine:
2x Honeywell TPE331-6-251M
Turboprop
Power:
776 HP
Max Cruise Speed:
295 Kts
546 Km/h
Approach Speed (Vref):
81 Kts
Travel range:
1,260 Nm
2,334 Kilometers
Service Ceiling:
29,590 feet
Rate of Climb:
2360 feet / minute
11.99meter / second
Take Off Distance:
661 meter - 2,168.61 feet
Landing Distance:
573 meter - 1,879.90 feet

Weight & dimensions

Max Take Off Weight:
5,250 Kg
11,574 lbs
Max Landing Weight:
5,000 Kg
11,023 lbs
Max Payload:
1,726 Kg
3,805 lbs
Fuel Tank Capacity:
367 gallon
1,389 liter
Baggage Volume:
1.2 m3 / 42 ft3

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Mitsubishi MU-2

The Mitsubishi MU-2 is a Japanese high-wing, twin-engine turboprop aircraft with a pressurized cabin manufactured by Mitsubishi Heavy Industries. It made its maiden flight in September 1963 and was produced until 1986. It is one of postwar Japan’s most successful aircraft, with 704 manufactured in Japan and San Angelo, Texas, in the United States.

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