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Yokosuka K4Y

From Wikipedia, the free encyclopedia
Japanese floatplane trainer
K4Y
RoleFloatplane trainer
Type of aircraft
National originJapan
ManufacturerYokosuka Naval Air Technical Arsenal
First flight1930
Introduction1933
Primary userImperial Japanese Navy Air Service
Number built211

TheYokosuka K4Y (orNavy Type 90 Seaplane Trainer) was aJapanesefloatplanetrainer of the 1930s. A single engined two-seatbiplane, 211 K4Ys were built between 1933 and 1940, serving as theImperial Japanese Navy's basic floatplane trainer throughout theSecond World War.

Development and design

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In 1930, theImperial Japanese Navy Air Service's basic seaplane trainer was theYokosuka K1Y or Type 13 Seaplane Trainer, which had been in use from 1925, and it instructed theFirst Naval Air Technical Arsenal based atYokosuka to design a replacement.[1] The design team, led byJiro Saha andTamefumi Suzuki designed asingle-baybiplane with a welded steel-tubefuselage and wooden wings, it being the first Japanese designed aircraft with such a fuselage.[2]

Yokosuka built two prototypes, powered by 90 hp (67 kW) Hatakaze four-cylinder air-cooledinline engines in 1930, flying in 1930, and after successful testing, a version powered by a 130 hpGasuden Jimpu[2] radial engine was ordered into production as theNavy Type 90 Seaplane trainer, with theshort designation K4Y1.[2]

Operational history

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Production began atWatanabe in May 1933, Watanabe building 156 by 1939, with production then transferring to Nippon Hikoki who built a further 53 in 1939–40.[3]

The K4Y1 started to replace the K1Y from 1933, remaining the Imperial Japanese Navy Air Service's principal basic seaplane trainer throughout the Pacific war. A few aircraft were released for civilian use.[2][3]

Units using this aircraft

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 Japan

Specifications (K4Y1 seaplane)

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Data fromJapanese Aircraft, 1910-1941[4]

General characteristics

  • Crew: 2
  • Length: 9.05 m (29 ft 8 in)
  • Wingspan: 10.90 m (35 ft 9 in)
  • Height: 3.51 m (11 ft 6 in)
  • Wing area: 29.5 m2 (318 sq ft)
  • Empty weight: 740 kg (1,631 lb)
  • Gross weight: 990 kg (2,183 lb)
  • Powerplant: 1 ×Gasuden Jimpu 2 seven-cylinder air-cooledradial engine, 97 kW (130 hp)

Performance

  • Maximum speed: 163 km/h (101 mph, 88 kn) at sea level
  • Cruise speed: 93 km/h (58 mph, 50 kn)
  • Range: 310 km (200 mi, 170 nmi)
  • Endurance: 3 hours 30 min
  • Service ceiling: 3,460 m (11,350 ft)
  • Time to altitude: 29 min 20 sec to 3,000 m (9,800 ft)

References

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Wikimedia Commons has media related toYokosuka K4Y.
Notes
  1. ^Mikesh & Abe 1990, pp. 273, 277
  2. ^abcdMikesh & Abe 1990, p. 277
  3. ^abFrancillon 1970, p. 494
  4. ^Mikesh & Abe 1990, pp. 277–278
Bibliography
  • Francillon, René J. (1970).Japanese Aircraft of the Pacific War. London: Putnam & Company Ltd.ISBN 0-370-00033-1.
  • Mikesh, Robert C.; Abe, Shorzoe (1990).Japanese Aircraft, 1910-1941. London: Putnam Aeronautical Books.ISBN 0-85177-840-2.
Torpedo bombers
Dive bombers
Reconnaissance seaplanes
Flying boats
Training aircraft
Transport aircraft
Special-purpose aircraft
Bombers
Land-based Reconnaissance
World War II Allied reporting names
Fighters (A)
Torpedo bombers (B)
Shipboard reconnaissance (C)
Dive bombers (D)
Reconnaissance seaplanes (E)
Observation seaplanes (F)
Land-based bombers (G)
Flying Boats (H)
Land-based Fighters (J)
Trainers (K)
Transports (L)
Special-purpose (M)1
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1 X as second letter is for experimental aircraft or imported technology demonstrators not intended for service,2 Hyphenated trailing letter (-J, -K, -L, -N or -S) denotes design modified for secondary role,3 Possibly incorrect designation, but used in many sources
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