Mitsubishi MU-2
Aircraft Information Mitsubishi MU-2
Mitsubishi MU-2 is a light twin-engine aircraft developed by the Japanese company Mitsubishi Heavy Industries in 1963. It was designed for use as a business aircraft and for regional passenger transportation.
The Mitsubishi MU-2 aircraft has a length of 11.7 meters, a wingspan of 11.9 meters, and a height of 4.3 meters. The maximum takeoff weight is 4,990 kg, and the maximum speed is 540 km/h. The range is approximately 2,500 km.
The MU-2 is equipped with two Pratt & Whitney Canada PT6A-20 turboprop engines, each with a power of 550 hp. The aircraft can carry up to 10 passengers depending on the cabin configuration.
The Mitsubishi MU-2 aircraft was produced in more than 700 units and was used in various countries for business flights, medical evacuations, and cargo transportation. However, due to several serious incidents, the production of the MU-2 was discontinued in 1986. Nevertheless, many MU-2 aircraft are still in operation.
Technical information about the Mitsubishi MU-2
- Length: 11.66 m
- Wingspan: 11.94 m
- Cabin dimensions: 1.37 m x 1.37 m x 3.05 m
- Maximum speed: 529 km/h
- Range: 2,222 km
- Empty weight: 2,200 kg
- Maximum weight: 4,000 kg
- Engine: 2 × Garrett TPE331-10-501M turboprop engines (each with 635 hp)
The most comfortable and safe places on the plane
Like in any other aircraft, the safest seats in the Mitsubishi MU-2 are located in the rear of the cabin as they are further away from the front where the engine is located. Additionally, seats near the cabin exits are also considered safe as they provide quicker access to the exit in case of an emergency.
As for comfort, the most comfortable seats in the Mitsubishi MU-2 are the ones by the windows as they offer a better view of the surrounding world and less engine noise. Additionally, seats in the first row of the cabin can also be comfortable as they provide more legroom and better access to onboard equipment. However, these seats may be less safe in case of an emergency as they are closer to the front of the aircraft.