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Fuji KM-2

General Aviation and Light Aircraft

The Fuji KM-2 is a Japanese propeller-driven light aircraft developed by Fuji Heavy Industries from the Beechcraft T-34 Mentor that Fuji built under licence, and various versions have served as primary trainers with the Japan Self-Defense Forces. The KM was a four-seat civil version of the LM-1 with the Lycoming engine later used on the LM-2, and the KM-2 that followed was a side-by-side two-seat trainer that first flew on 16 January 1962. The Japan Maritime Self-Defense Force bought sixty-two as primary trainers and the Ground Self-Defense Force bought two as the TL-1, and its tandem-cockpit development, the KM-2B, became the Fuji T-3.

Facts
Year
1962 1
Engine Class
Piston 1
Power (kW)
250 1
Top Speed (km/h)
378 1
Mass (kg)
1134 1
Maximum Mass (kg)
1750 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Fuji KM-2 (Wikipedia)

Of Make

Source Fuji KM-2 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Fuji KM-2 (Wikipedia)Lead
Quote, Lead
The Fuji KM-2 is a Japanese propeller-driven light aircraft, which was developed by Fuji Heavy Industries from the Beechcraft T-34 Mentor which Fuji built under licence.

Originated In

Also in Geography Atlas: where this subject originated.

Source Fuji KM-2 (Wikipedia)Lead
Quote, Lead
The Fuji KM-2 is a Japanese propeller-driven light aircraft, which was developed by Fuji Heavy Industries from the Beechcraft T-34 Mentor which Fuji built under licence.
Sources
1. Fuji KM-2 (Wikipedia)
  • Design and development
    the KM-2 was developed as a side-by-side two-seat trainer, first flying on 16 January 1962.
  • Lead
    The Fuji KM-2 is a Japanese propeller-driven light aircraft, which was developed by Fuji Heavy Industries from the Beechcraft T-34 Mentor which Fuji built under licence.
  • Specifications (KM-2)
    Lycoming IGSO-480-A1A6 air-cooled flat-six engine, 250 kW (340 hp)
  • Specifications (KM-2), mass
    Empty weight: 1,134 kg (2,500 lb)
  • Specifications (KM-2), maximum mass
    Max takeoff weight: 1,750 kg (3,858 lb)
  • Specifications (KM-2), top speed
    Maximum speed: 378 km/h (235 mph, 204 kn) at 4,880 m (16,000 ft)
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