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Tachikawa Ki-54

From Wikipedia, the free encyclopedia

Ki-54
Tachikawa Ki-54
Role Twin-engine advanced crew trainer
Manufacturer Tachikawa Aircraft Company Ltd
Designer Shinjiro Shinagawa
First flight Summer 1940
Introduction 1941
Retired 1945 (Japan)
1952 (China)
Primary user Imperial Japanese Army Air Force
Produced 1941-1945
Number built 1,368

The Tachikawa Ki-54 was a Japanese twin-engine advanced trainer used during World War II. The aircraft was named Hickory by the Allies.

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Transcription

History

The Ki-54 was developed in response to an Imperial Japanese Army requirement for a twin-engine advanced trainer, principally for crew training. The prototype first flew in summer 1940 and, on completing trials, entered production in 1941 as Army Type 1 Advanced Trainer Model A (Ki-54a). The Ki-54a was soon followed by the Ki-54b as Army Type 1 Operations Trainer Model B and Ki-54c as Army Type 1 Transport Model C. The Ki-54b and -c enjoyed successful careers until the end of the war. A few captured aircraft were flown after the war by various users.

Operators

 Japan
 Manchukuo
China-Nanjing
 China
 China
 French Indochina
 United Kingdom

Variants

  • Ki-54a - unarmed pilot trainer
  • Ki-54b - armed crew trainer
  • Ki-54c - eight-passenger light transport, communications aircraft. Civil designation Y-59.
  • Ki-54d - maritime reconnaissance/ASW, carried 8x 60-kg (132-lb) depth charges
  • Ki-110 - one prototype Ki-54c of all-wood construction, destroyed in US bombing attack
  • Ki-111 - projected fuel tanker (none built)
  • Ki-114 - projected fuel tanker of all-wood construction (none built)

Surviving aircraft

Ki-54 at the Misawa Aviation & Science Museum

Specifications (Ki-54c light transport)

Data from The Concise Guide to Axis Aircraft of World War II;[7] Japanese Aircraft of the Pacific War[8]

General characteristics

  • Crew: 2
  • Capacity: 8
  • Length: 11.94 m (39 ft 2 in)
  • Wingspan: 17.9 m (58 ft 9 in)
  • Height: 3.58 m (11 ft 9 in)
  • Wing area: 40 m2 (430 sq ft)
  • Empty weight: 2,954 kg (6,512 lb)
  • Gross weight: 3,897 kg (8,591 lb)
  • Powerplant: 2 × Hitachi Ha13a (Army Type 98 450hp Air Cooled Radial) 9-cylinder air-cooled radial piston engine, 380 kW (510 hp) each for take-off
350 kW (470 hp) at 1,700 m (5,600 ft)
  • Propellers: 2-bladed metal propeller

Performance

  • Maximum speed: 375 km/h (233 mph, 202 kn)
  • Cruise speed: 240 km/h (150 mph, 130 kn)
  • Range: 960 km (600 mi, 520 nmi)
  • Service ceiling: 7,180 m (23,560 ft)
  • Wing loading: 97.4 kg/m2 (19.9 lb/sq ft)
  • Power/mass: 0.195 kW/kg (0.119 hp/lb)

See also

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ^ Thomas, Andy (July 2008). "Vietnam Prelude". FlyPast. Stamford, Lincolnshire, England: Key Publishing (324): 70–71.
  2. ^ "Anyone got pics of the AWM Ki-54?". Warbirdz Aviation Photography. Archived from the original on 12 April 2012. Retrieved 15 December 2013.
  3. ^ "Tachikawa Ki-54c 'Hickory' fuselage: 10th Independent Air Brigade, Imperial Japanese Army Air Force". awm.gov.au. Australian War Memorial. Retrieved June 15, 2018.
  4. ^ "Aircraft database". LPH2O. April 3, 2016.
  5. ^ "旧陸軍の練習機69年ぶり地上に、青森・十和田湖で引き揚げ" [Former Army training aircraft pulled out of lake for the first time in 69 years] (in Japanese). September 5, 2012. Retrieved April 2, 2016.
  6. ^ "旧陸軍練習機、十和田湖で発見…戦時中に墜落". Yomiuri Online (in Japanese). August 13, 2010. Archived from the original on August 16, 2010.
  7. ^ Mondey 1996, p. ?.
  8. ^ Francillon 1979, p. 256.

Bibliography

This page was last edited on 21 November 2023, at 15:15
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