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Aichi F1A

From Wikipedia, the free encyclopedia
Japanese reconnaissance floatplane
F1A
General information
TypeReconnaissancefloatplane
National originEmpire of Japan
ManufacturerAichi
Number built2
History
First flight1936

TheAichi F1A (designatedAB-13 by its designers and manufacturers atAichi) was a prototypeJapanesefloatplane of the 1930s. A single-enginedbiplane, the F1A was intended as a short-range observation aircraft suitable for operation off theImperial Japanese navy's warships, but only two were built, theMitsubishi F1M being selected instead.

Design and development

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The F1A was designed byAichi in response to a 1935 specification, issued to Aichi,Kawanishi andMitsubishi for a replacement for theImperial Japanese Navy'sNakajima E8Nfloatplanes, which were used for short-ranged reconnaissance and observation missions from the Navy's warships. Aichi at first considered a low-wingedmonoplane design, theAM-10, to meet this requirement, but this was rejected in favour of a more conventionalbiplane design, theAB-13.[1][2]

The AB-13 was a small single-bay biplane of mixed construction. It had woodenstressed-skin wings withplywood skinning thatfolded to allow easy storage aboard ship, while combat flaps were fitted as the aircraft was required to have sufficient maneuverability for air combat as well as its normal observation missions. The fuselage was of metal construction, with the pilot sitting in an open cockpit, but the observer's position being enclosed. Both float and wheeled undercarriages were designed, with the seaplane having a single main float, while the landplane version had a fixedtailwheel undercarriage. Power was provided by a singleNakajima Hikariradial engine.[3]

Operational history

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Two prototypes of the AB-13, designatedExperimental 10-Shi[a] Observation Aircraft and with theshort system designation F1A were built, the first a floatplane and the second with wheeled undercarriage, both being completed in 1936.[3] Although Mitsubishi's competingF1M1 prototypes had poor stability both on the water and in the air, they had superior performance to Aichi's design. Mitsubishi redesigned its aircraft as the F1M2, eliminating its handling problems,[4] and it was selected for production in 1940.[5]

Specifications (Floatplane)

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Data fromJapanese Aircraft, 1910–1941[5]

General characteristics

  • Crew: 2
  • Length: 9.30 m (30 ft 6 in)
  • Wingspan: 11.00 m (36 ft 1 in)
  • Height: 4.10 m (13 ft 5 in)
  • Wing area: 28.0 m2 (301.399 sq ft)
  • Empty weight: 1,400 kg (3,086 lb)
  • Gross weight: 2,100 kg (4,629 lb)
  • Max takeoff weight: 2,380 kg (5,247 lb)
  • Powerplant: 1 ×Nakajima Hikari 1 nine-cylinder air-cooledradial engine, 610 kW (820 hp)

Performance

  • Maximum speed: 386 km/h (240 mph, 207.8 kn) at 3,000 m (9,840 ft)
  • Stall speed: 95.4 km/h (59.3 mph, 51.5 kn)
  • Range: 1,449 km (900 mi, 783 nmi) at 185 km/h (100 knots, 115 mph)
  • Endurance: 8 hr 30 min
  • Service ceiling: 9,275 m (30,430 ft)
  • Time to altitude: 3,000 m (9,840 ft) in 4 min 26 s

Armament

  • Guns: 2× fixed forward firing 7.7 mm machine guns, 1 machine gun in rear cockpit

References

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Footnotes
  • a In the Japanese Navy designation system, specifications were given aShi number based on the year of the Emperor's reign it was issued. In this case 10-Shi stood for 1935, the 10th year of theShōwa era.[6]
Citations
  1. ^Mikesh and Abe 1990, p. 77.
  2. ^Francillon 1970, p. 358.
  3. ^abMikesh and Abe 1990, pp. 77–78.
  4. ^Francillon 1970, pp. 358–359.
  5. ^abMikesh and Abe 1990, p. 78.
  6. ^Mikesh and Abe 1990, pp. 2, 286.
Bibliography
  • Francillon, Ph.D., René J.Japanese Aircraft of the Pacific War. London: Putnam & Company Ltd., 1970.ISBN 0-370-00033-1 (2nd edition 1979,ISBN 0-370-30251-6).
  • Mikesh, Robert C. and Shorzoe Abe.Japanese Aircraft, 1910–1941. London: Putnam Aeronautical, 1990.ISBN 0-85177-840-2.


External links

[edit]
Aichi aircraft
Manufacturer
designations
Imperial Japanese Navy
short designations
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
Floatplane fighters (N)
Land-based bombers (P)
Patrol (Q)
Land-based reconnaissance (R)
Night fighters (S)
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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