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Fuji LM-1 Nikko

General Aviation and Light Aircraft

The Fuji LM-1 Nikko was a Japanese four-seat light communications aircraft of the 1950s. Fuji Heavy Industries had built 176 Beech T-34 Mentor trainers under licence in the early 1950s and then redesigned the Mentor as a communications aircraft by adding a lengthened centre fuselage to the Mentor wing, undercarriage and tail. Twenty-seven LM-1s with a 225 hp Continental engine were produced in 1955 and 1956 for the Japan Air Self-Defense Force, where they were used for communications and general duties, and after withdrawal several were sold on the US civil market and are flown as warbirds. The higher-powered LM-2 with a 340 hp Lycoming engine followed, with two built.

Facts
Year
1955 1
Status
Out of production 1
Power (kW)
168 1
Units Built
27 1
Top Speed (km/h)
298 1
Mass (kg)
1013 1
Maximum Mass (kg)
1531 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Fuji LM-1 Nikko (Wikipedia)

Of Make

Source Fuji LM-1 Nikko (Wikipedia)
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Manufactured By

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Source Fuji LM-1 Nikko (Wikipedia)Lead
Quote, Lead
The Fuji LM-1 Nikko is a Japanese light communications aircraft of the 1950s.

Originated In

Also in Geography Atlas: where this subject originated.

Source Fuji LM-1 Nikko (Wikipedia)Lead
Quote, Lead
The Fuji LM-1 Nikko is a Japanese light communications aircraft of the 1950s.
Sources
1. Fuji LM-1 Nikko (Wikipedia)
  • Development
    27 LM-1s were produced during 1955
  • Operational history
    After withdrawal from operation, several LM-1s were sold on the U.S. civil market and are flown by civil pilots as "warbirds".
  • Lead
    The Fuji LM-1 Nikko is a Japanese light communications aircraft of the 1950s.
  • Variants
    225 h.p. (168 kW) Continental engine (27 built)
  • Specifications (LM-1)
    Empty weight: 2,234 lb (1,013 kg)
  • Specifications (LM-1), maximum mass
    Gross weight: 3,375 lb (1,531 kg)
  • Specifications (LM-1), top speed
    Maximum speed: 185 mph (298 km/h, 161 kn)
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