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Hitachi TR.1

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TR.1 and TR.2
Role Airliner
National origin Japan
Manufacturer Hitachi
First flight 8 April 1938
Number built 13

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.

The TR.2 was a revised and strengthened design with a larger wing area, and main undercarriage that only semi-retracted. Twelve examples were built in a small series, but performance was not as good as the TR.1, since the modifications to the design had added 260 kg (570 lb) to the aircraft.


Specifications (TR.1)

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Data from Japanese Aircraft 1910–1941[1]

General characteristics

  • Crew: 2
  • Capacity: 6 passengers
  • Length: 10.60 m (34 ft 9 in)
  • Wingspan: 14.10 m (46 ft 3 in)
  • Height: 3.50 m (11 ft 6 in) (to top of radio mast)
  • Wing area: 24.5 m2 (264 sq ft)
  • Empty weight: 1,910 kg (4,211 lb)
  • Gross weight: 3,000 kg (6,614 lb)
  • Powerplant: 2 × Gasuden Jimpu 5A nine-cylinder air-cooled radial engine, 180 kW (240 hp) each

Performance

  • Maximum speed: 303 km/h (188 mph, 163 kn)
  • Cruise speed: 251 km/h (156 mph, 136 kn)
  • Range: 1,516 km (942 mi, 819 nmi)
  • Service ceiling: 4,380 m (14,370 ft)
  • Time to altitude: 14 min 47 s to 3,000 m (9,800 ft)

References

[edit]
  • Mikesh, Robert C.; Abe, Shorzoe (1990). Japanese Aircraft 1910–1941. London: Putnam. ISBN 0-85177-840-2.
  • The Illustrated Encyclopedia of Aircraft. London: Aerospace Publishing. p. 2174.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 511.