The Fuji FA-200 Aero Subaru is a single-engine piston-powered monoplane built by Fuji Heavy Industries of Japan. Design and development Fuji Heavy Industries began development of a four-seat light aeroplane, the Fuji FA-200 Aero Subaru in 1964, the first prototype flying on 12 August 1965. It is a low-wing all-metal aircraft, fitted with a fixed nosewheel undercarriage and a sliding canopy. It was first certified in Japan on 6 July 1966, with certification in the United States occurring on 26 September 1967. Production started in March 1968, continuing until 1986, with a total of 275 built. Variants F-200-II Prototype with a Lycoming O-320 engine FA-200-160 Initial version, powered by 120 kW Lycoming O-320 engine and fixed-pitch propeller. FA-200-180 More powerful development - Lycoming IO-360 engine and constant speed propeller. FA-200-180AO Powered by 130 kW Lycoming IO-320 engine and fitted with fixed-pitch propeller. FA-203-S Experimental short takeoff and landing (STOL) version, developed by Japan's National Aerospace Laboratory fitted with boundary layer control system. F-201 Proposed three-seat variant, not built. F-202 Proposed two-seat aerobatic variant, not built. F-203 Proposed STOL variant. F-204 Proposed crop spraying variant, not built. Accidents and incidents On May 13, 2017, a Fuji FM 200-160 with tail number E7-AAS, crashed in Jasenica, near Mostar in Bosnia and Herzegovina, killing all 5 on board. Among them were 3 children. Specifications (FA-200-180) See also References External links FUJI/FA-200 AERO SUBARU Subaru FA-200 1960s Japanese civil utility aircraft Single-engined tractor aircraft Low-wing aircraft Aircraft first flown in 1965