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Fuji T-3

General Aviation and Light Aircraft

The Fuji T-3 was a primary military trainer built by Fuji Heavy Industries for the Japan Air Self-Defense Force, a development of the four-seat KM-2 that combined its structure and Lycoming engine with the tandem cockpit of the Beechcraft T-34 Mentor, first flying on 17 January 1978. Fifty were bought and production continued until 1982, and the type served with the 11th and 12th flight training wings until it was retired in 2007 and replaced by the turboprop Fuji T-7. A 254 kW Lycoming IGSO-480 six-cylinder piston engine drove a three-bladed constant-speed propeller on an airframe weighing 1,120 kg empty and 1,510 kg at maximum take-off.

Facts
Year
1978 1
Engine Class
Piston 1
Status
Out of production 1
Power (kW)
254 1
Units Built
50 1
Mass (kg)
1120 1
Maximum Mass (kg)
1510 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Fuji T-3 (Wikipedia)

Of Make

Source Fuji T-3 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Fuji T-3 (Wikipedia)Lead, body style
Quote, Lead, body style
The Fuji T-3 is a primary military trainer aircraft used by the Japan Air Self Defense Force, manufactured by Fuji Heavy Industries.

Originated In

Also in Geography Atlas: where this subject originated.

Source Fuji T-3 (Wikipedia)Lead, body style
Quote, Lead, body style
The Fuji T-3 is a primary military trainer aircraft used by the Japan Air Self Defense Force, manufactured by Fuji Heavy Industries.
Sources
1. Fuji T-3 (Wikipedia)
  • Lead
    Its first flight was in 1978.
  • Lead, units built
    In the course of its service life, 50 units were produced.
  • Operational history
    The T-3 was retired in 2007 and replaced by the Fuji T-7, a turboprop variant of the T-3
  • Lead, body style
    The Fuji T-3 is a primary military trainer aircraft used by the Japan Air Self Defense Force, manufactured by Fuji Heavy Industries.
  • Specifications (T-3)
    Lycoming IGSO-480 6-cylinder horizontally opposed air-cooled piston engine, 254 kW (341 hp)
  • Specifications (T-3), mass
    Empty weight: 1,120 kg (2,469 lb)
  • Specifications (T-3), maximum mass
    Max takeoff weight: 1,510 kg (3,329 lb)
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