Mitsubishi MU-2

Twin Turboprops

ICAO aircraft code MU2

Manufacturer Mitsubishi Heavy Industries

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

Full description

Incorrect info? Let us know

Similar aircraft

Cessna 340

Cessna 320 Skyknight

Swearingen Merlin

Diamond DA-42 Twin Star

Mitsubishi MU-2 specifications

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.