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Fuji FA-200 Aero Subaru

General Aviation and Light Aircraft

The Fuji FA-200 Aero Subaru is a single-engine piston-powered monoplane built by Fuji Heavy Industries of Japan, a four-seat low-wing all-metal light aeroplane with a fixed undercarriage. Development began in 1964 and the first prototype flew on 12 August 1965; it was certified in Japan on 6 July 1966 and in the United States on 26 September 1967. Production started in March 1968 and continued until 1986 with a total of 275 built, in versions from the FA-200-160 with a 160 hp Lycoming O-320 and fixed-pitch propeller to the FA-200-180 with a 180 hp Lycoming IO-360 and constant-speed propeller, plus the experimental FA-203-S short take-off and landing version.

Facts
Year
1965 1
Propulsion
Piston engine 1
Engine Class
Piston 1
Status
Out of production 1
Power (kW)
130 1
Units Built
275 1
Top Speed (km/h)
233 1
Mass (kg)
650 1
Maximum Mass (kg)
1150 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Fuji FA-200 Aero Subaru (Wikipedia)

Of Make

Source Fuji FA-200 Aero Subaru (Wikipedia)
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Manufactured By

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Source Fuji FA-200 Aero Subaru (Wikipedia)Lead
Quote, Lead
The Fuji FA-200 Aero Subaru is a single-engine piston-powered monoplane built by Fuji Heavy Industries of Japan.

Originated In

Also in Geography Atlas: where this subject originated.

Source Fuji FA-200 Aero Subaru (Wikipedia)Lead
Quote, Lead
The Fuji FA-200 Aero Subaru is a single-engine piston-powered monoplane built by Fuji Heavy Industries of Japan.
Sources
1. Fuji FA-200 Aero Subaru (Wikipedia)
  • Design and development
    the first prototype flying on 12 August 1965.
  • Design and development, units built
    Production started in March 1968, continuing until 1986, with a total of 275 built.
  • Lead
    The Fuji FA-200 Aero Subaru is a single-engine piston-powered monoplane built by Fuji Heavy Industries of Japan.
  • Specifications (FA-200-180)
    Lycoming IO-360B1B four cylinder air-cooled horizontally-opposed piston engine, 130 kW (180 hp)
  • Specifications (FA-200-180), mass
    Empty weight: 650 kg (1,433 lb)
  • Specifications (FA-200-180), maximum mass
    Max takeoff weight: 1,150 kg (2,535 lb)
  • Specifications (FA-200-180), top speed
    Maximum speed: 233 km/h (145 mph, 126 kn)
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