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
Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Fuji LM-1 Nikko (Wikipedia)
Of Make
Source Fuji LM-1 Nikko (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Fuji LM-1 Nikko (Wikipedia)LeadQuote, 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)LeadQuote, 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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