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Mitsubishi MU-2

The Mitsubishi MU-2 is a Japanese high-wing, twin-engined, 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.

Design and development
Work on the MU-2, Mitsubishi's first postwar aircraft design, began in 1956. Designed as a light twin turboprop transport suitable for a variety of civil and military roles, the MU-2 first flew on 14 September 1963. This first MU-2, and the three MU-2As built, were powered by the Turbomeca Astazou turboprop. Civil MU-2s powered by Garrett engines were certified as variants of the MU-2B, using the MU-2B type followed by a number. For marketing purposes, each variant was given a suffix letter; the MU-2B-10, for example, was sold as the MU-2D, while the MU-2B-36A was marketed as the MU-2N. The MU-2 has a high cruise speed coupled with a low landing speed. This is accomplished by using over-wing spoilers instead of conventional ailerons for roll control, allowing the use of full-span, double-slotted flaps on the trailing edge of the wing; the very large flaps give the MU-2 wing loading comparable to a Beechcraft King Air in landing configuration, while having wing loading comparable to a light jet in cruise. The spoilers are highly effective, even when the MU-2 wing is stalled, and the lack of ailerons eliminates adverse yaw. The last Japanese-built aircraft was completed in January 1987. The subsequent production aircraft, designated MU-2B, were delivered with the Garrett TPE331 engines that remained standard on all later models. Thirty-four MU-2Bs were built, followed by 18 examples of the similar MU-2D. The Japanese armed forces purchased four unpressurized MU-2Cs and 16 search-and-rescue variants designated MU-2E. Featuring slightly more powerful, upgraded TPE331 engines, 95 examples of the MU-2F were sold. : This MU-2 is operated in a medivac configuration by Thunder Airlines of Thunder Bay, Canada. Beginning with the MU-2G, the fuselage was stretched. The MU-2M, of which only 28 were built, is regarded as the toughest and most desired of all short-bodied MU-2s, especially with a −10 engine conversion. It had a short fuselage and the same engines as the MU-2K and stretched MU-2J, and had an increase in cabin pressurization to 6.0 psi; it was followed by the MU-2P, which had newer, four-blade propellers. The final short-fuselage MU-2s produced were known as Solitaires and were fitted with Garrett TPE331-10-501M engines. The first significant change to the airframe came with the stretched MU-2G, first flying 10 January 1969, which featured a 1.91 m (6 ft 3 in) longer fuselage than earlier models; 46 were built before being succeeded by the more powerful MU-2J (108 constructed). The MU-2L (29 built) was a higher-gross-weight variant, followed by the MU-2N (39 built) with uprated engines and four-blade propellers. The final stretched-fuselage MU-2 was named the Marquise, and like the Solitaire, used TPE331 engines. ==Operational history==
Operational history
Military service Japan . The Japan Self-Defense Forces are the only military operators to have flown the MU-2 in front-line service. Ground Self-Defense Force The four C-model aircraft built, in addition to 16 MU-2Ks, entered service with the Japan Ground Self-Defense Force (JGSDF) with the designation LR-1; they were used as liaison and photo-reconnaissance aircraft. They were retired in 2016. A number of them have been placed as gate guardians at JGSDF bases. Air Self-Defense Force Twenty-nine MU-2Es were purchased by the Japan Air Self-Defense Forces as search-and-rescue aircraft and designated MU-2S. Additional equipment consisted of a "thimble" nose radome, increased fuel capacity, bulged observation windows, and a sliding door for dropping rafts. Argentina Four civilian MU-2 (LV-MCV, LV-MOP, LV-OAN, and LV-ODZ) were acquired by the Argentine Air Force during the Falkland War. These Mitsubishis were unarmed, but used during combat operations by the Escuadrón Fénix as pathfinders, reconnaissance, and communications-relay planes. One of their missions was flying as guiding planes to the IA-58 Pucará replacements required after losses on the raid on Pebble Island. New Zealand In late 2009, the Royal New Zealand Air Force (RNZAF) took delivery of four Mitsubishi MU-2F fixed-wing training aircraft from the United States for use as training aids. In New Zealand service, they are known as the Mitsubishi MU-2 Sumo. The aircraft were ferried to New Zealand and are located at the RNZAF's Ground Training Wing (GTW) at RNZAF Base Woodbourne near Blenheim in New Zealand's South Island. United States Since 1987, MU-2s have been flown by retired United States Air Force (USAF) pilots working under government contract at Tyndall Air Force Base, Florida, where they provide USAF undergraduate air battle manager students of the USAF Weapons Controller School with their initial experience controlling live aircraft. In the tactical simulations, the aircraft usually represent F-15s and Mikoyan MiG-29s. Students must control eight MU-2 missions before they can progress to controlling high-performance aircraft such as F-15s or F-22s. Flight around the world On 25 August 2013, Mike Laver, owner and pilot of N50ET (a −10 engine converted 1974 K-model equipped with five-bladed MT-composite propellers, which had just received a supplemental type certificate (STC) under Air First of Aiken, South Carolina), along with AOPA Pilot technical editor Mike Collins, embarked on an around-the-world journey in the MU-2B-25. The voyage commenced at Aiken Municipal Airport (now Aiken Regional Airport) and visited Nagoya, Japan, on 14 September 2013, the 50th anniversary of the MU-2. Safety concerns In the United States, the MU-2 had a spotty safety record during its early decades, as its high performance coupled with a relatively low purchase price appealed to amateur pilots who did not appreciate how demanding it is to fly compared to slower piston engined aircraft. The absence of adverse yaw eliminates the need to use rudder for coordinated flight, but proper and prompt use of rudder is vital to counter the aircraft's tendency to roll in reaction to engine torque; at low airspeed, the aircraft will rapidly roll and enter an accelerated stall if the pilot applies full power without adequate preparation, and safe recovery from this condition is very difficult at low altitude. Most crashes early in the type's service life were attributable to pilot error, but in 1981, four uncontrolled descents from altitude prompted the United States National Transportation Safety Board (NTSB) to initiate separate investigations into the cabin pressurization system and autopilot, but the outcome was inconclusive. In 1983, after more crashes, the NTSB convinced the Federal Aviation Administration (FAA) to perform a more comprehensive study of various aircraft systems; the study ultimately did not fault the MU-2's design, but the repeated investigations had damaged the aircraft's reputation by this time. This prompted Mitsubishi, in cooperation with FlightSafety International, to initiate the Pilot's Review of Proficiency (PROP) seminar program to better educate MU-2 pilots about the aircraft's characteristics. The PROP seminars were suspended following the end of MU-2 production in 1986, but were reinstated in 1994 due to continuing accidents. By 2011, the SFAR was credited with lowering MU-2 accident rates below those for similar turboprop aircraft. Additionally, although some owners had worried that the SFAR would depress aircraft prices even further, resale values rebounded as potential owners recognized that the aircraft is very safe with a properly trained pilot. Despite these early problems, aviation experts have characterized the MU-2 as being robustly designed and constructed, and relatively few MU-2 crashes have been directly attributed to mechanical or structural failures. ==Variants==
Variants
Short fuselage ;XMU-2 :Astazou-powered prototype, 1 built ;MU-2A :Prototypes powered by Turbomeca Astazou IIK engines, 3 built. ;MU-2B :Production variant powered by Garrett TPE331-25A engines. 34 built. ;MU-2C (MU-2B-10) :Unpressurized variant for the Japan Ground Self-Defense Force, 4 built. ;MU-2D (MU-2B-10) :Improved MU-2B, higher operating altitude and bladder fuel tanks rather than wet-wings, 18 built. ;MU-2DP (MU-2B-15) :MU-2D with 90-gallon tip tanks and upgraded engines, 3 built. ;MU-2E :Unpressurized variant for the Japanese military designated MU-2S ;MU-2F (MU-2B-20) :Variant with improved engines and 90-gallon tip tanks as MU-2DP but certified at a higher gross weight and additional fuel tanks, 95 built. ;MU-2K (MU-2B-25) :Short fuselage variant of the MU-2J, 83 built. ;MU-2M (MU-2B-26) :Revised variant of the MU-2K with increased weight, and increased cabin pressure, 27 built. ;MU-2P (MU-2B-26A) :Improved variant with four-bladed propellers and improvements as MU-2N, 31 built. ;Solitaire (MU-2B-40) :Variant with improved engines and increased fuel capacity, 57 built between 1979 and 1985. Long fuselage ;MU-2G (MU-2B-30) :Stretched variant with a 1.91m increase in length, larger cabin and change to landing gear configuration, first flown in January 1969, 46 built. ;MU-2J (MU-2B-35) :Variant with improved engines, eleven inch increase in cabin length and increased gross weight, 108 built. ; :Revised variant of the MU-2L with increased weight, and increased cabin pressure. ; :Improved variant with four-bladed propellers and other improvements including an extra cabin window, 36 built. ; :Variant with improved engines, 139 built. ;Cavenaugh Cargoliner :Freighter conversions of long fuselage MU-2 variants by Cavenaugh Aviation Inc. of Conroe, Texas, by addition of a crew door in place of a flight deck window and a large cargo door in the rear port fuselage. Eleven aircraft had been converted by March 1987. Military ;LR-1 :Japanese military designation for MU-2C and MU-2Ks operated by the JGSDF, 20 delivered. ;MU-2S :Japanese military designation for a MU-2E search and rescue variant for the air force, 29 delivered. ==Aircraft on display==
Aircraft on display
;Australia • An MU-2 is on display at the Australian Aviation Heritage Centre at Darwin International Airport in Darwin, Australia. ;Japan • An MU-2 (registration: JA8628) is on display at the Museum of Aeronautical Sciences in Narita International Airport in Narita, Japan. ;Mexico • An MU-2P (code ETE-1357) is on display at the Museo Militar de Aviacion at the Felipe Ángeles International Airport in Santa Lucia, Mexico. ;United States • An MU-2 is on display at Sparks Aviation at the Tulsa International Airport in Tulsa, Oklahoma, in the United States. ==Incidents and accidents==
Incidents and accidents
As of April 2025, 172 documented crashes and 400 deaths have involved the MU-2. • On 19 April 1993, an MU-2B-60 owned by the State of South Dakota, registration number N86SD, sustained extensive damage to the fuselage and left-hand wing and engine mounts after a propeller blade separation during cruise. The pilot was unable to maintain altitude and crashed into a farm silo in low visibility about south of Dubuque, Iowa. All eight people aboard the aircraft died, including George S. Mickelson, then governor of South Dakota. Later that April, investigators' findings prompted the FAA to order the immediate inspection of Hartzell propellers similar to those on the accident aircraft. • On 10 November 2013, Perry Inhofe, son of U.S. Senator Jim Inhofe, died when the MU-2 he was flying crashed in Owasso, Oklahoma. Inhofe was the sole occupant of the aircraft. • On 29 March 2016, an MU-2B-60 operated by Aero Teknic, a Canadian aircraft maintenance company, crashed on approach to Îles-de-la-Madeleine Airport, killing all seven people aboard, including former Canadian politician Jean Lapierre, his family, and the two pilots. An initial survivor died of a heart attack after being pulled from the wreckage. The Transportation Safety Board of Canada investigated the crash and determined that the pilot's decision to continue an unstable approach resulted in loss of control during final approach. ==Specifications (MU-2L)==
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