Fuji FA-200 Aero Subaru

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 undercarriage. 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.{{cite book|editor=Donald, David|title = The Encyclopedia of World Aircraft|year = 1997 ==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 O-360-A5AD 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)==