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TR.1 and TR.2

Hitachi · Commercial · Japan · Interwar (1919–1938)

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The Hitachi TR.1 was a small airliner developed in Japan in 1938, produced in small numbers as the TR.2. It was a low-wing, cantilever monoplane with retractable tailwheel undercarriage and a fully enclosed cabin. The design strongly resembled the Airspeed Envoy that it was intended to replace in Japanese airline service. Testing of the TR.1 prototype commenced on 8 April 1938 at Haneda Airport, but it suffered a serious accident on 22 June due to a landing in which one of the main undercarriage units failed to extend.

Specifications

Category
Fixed Wing
Sub-Category
Commercial
Domain
Civil
Era
Interwar (1919–1938)
Country
Japan
Manufacturer
Hitachi
Service Entry
1938
Produced
13
Engine
2× nine-cylinder air-cooled radial engine
Thrust / Power
240 hp each
Length (ft)
35
Wingspan (ft)
46
Empty Weight (lb)
4211
MTOW (lb)
6614
Service Ceiling (ft)
14370
Range (mi)
942
Max Speed (mph)
188