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Inexperience with the MU-2s higher speeds, altitudes, and climb and descent rates resulted in many crashes. In Europe, pilots were required to obtain a specific type rating to fly the MU-2, resulting in roughly half the accident rate of early operations in the U.S.
With flap extension, the surface area of the wing increases by around 21%, thus lowering the wing loading and the stall speeds. Typical approach speeds range between 101 and 109 KCAS.
Much of the noise of a propeller aircraft is of aerodynamic origin due to the flow of air around the blades. The helicopter main and tail rotors also give rise to aerodynamic noise. This type of aerodynamic noise is mostly low frequency determined by the rotor speed.
Quite many small airplanes dont have mufflers in order to save on costs, space, engine performance, weight and additional maintenance. But equally, quite many small airplanes have mufflers for additional reasons related to the exhaust temperatures and yet emit excessive amounts of noise.
The Mitsubishi MU-2 is a high-performance turboprop with an extraordinary top speed of 370 mph. It can cruise at an exceptional 360 mph. Much of this outstanding performance apparently is the result of rather compact overall dimensions for a turboprop twin.
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The exhaust pipes on the MU2 are mere inches in length, and when it is operating on the ramp, it will blow your brains out with noise. It is always interesting to see people mill around the airplane as I start but quickly head for shelter after I start up.
Landing distance (50) 2,200. The Mitsubishi MU-2 is a high-performance turboprop with an extraordinary top speed of 370 mph. It can cruise at an exceptional 360 mph. Much of this outstanding performance apparently is the result of rather compact overall dimensions for a turboprop twin.
MU2. The Mitsubishi MU-2 is a high-wing, twin-engine turboprop, and has a pressurized cabin. MU-2: 2 x 605 SHP Garrett TPE331-25A or 2 x 724 SHP Garrett TPE331-G-251M turboprops with 3 blade propellers.
Stall speed clean was 98 mph which was reduced to 74 mph with the full 40 of flaps deployed. The MU-2B10 or D model was the next evolution off the drawing board. With the D, the maximum operating altitude increase from 23,000 to 25,000 feet while maintaining a cabin pressure of 8,000 feet.
Max Ramp Weight 10,520 lbs. 10,520 lbs. 10,520 lbs. Useful Load 3,590 lbs.

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