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Curtiss A-12 Shrike

From Wikipedia, the free encyclopedia
American attack aircraft
Not to be confused withLockheed A-12 orMcDonnell Douglas A-12 Avenger II.

A-12 Shrike
General information
TypeGround-attack aircraft
ManufacturerCurtiss
Primary usersUnited States Army Air Corps
Number built46[1]
History
Introduction date1933
Retired1942
Developed fromXA-8 Shrike
YA-10 Shrike

TheCurtiss A-12 Shrike was theUnited States Army Air Corps' secondmonoplaneground-attack aircraft, and its main attack aircraft through most of the 1930s. It was based on theA-8, but had aradial engine instead of the A-8's inline,water-cooled engine, as well as other changes.

Design and development

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Formation of Curtiss A-12 Shrikes during exercises near Wheeler Field, Oahu, Hawaii circa 1940.

TheModel 60 was developed from advancements of theA-8 and the experimentalYA-10. However, it became obsolete after a short use period, mainly because of fast-improving aviationtechnology, as well as the USAAC's desire for multi-engined attack aircraft.[2]

The most obvious difference between the A-12 and the A-8 is the air-cooled, radial engine in the A-12, which replaced the A-8'sinline, water-cooled engine. This was a response to the USAAC's move toward a preference for radial engines, especially in attack aircraft. The rationale behind this preference is that the radial engine has a lower profile, making it less vulnerable to ground fire, and a simpler cooling mechanism, which is also less prone to groundfire, as well as overall maintenance problems.[2]

These aircraft retained the opencockpit introduced in theA-8 production batch, and carried the same weapons load. In an attempt to improve pilot/observer co-operation, the rear cockpit was moved forward sufficiently for its glazed covering to form a continuation of the fuselage decking behind the pilot's cockpit.[3]

NineUSAAF A-12s were still in service atHickam Field on7 December 1941, but they saw no combat.[4]

Operational history

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On 15 August 1937, during the start of theSino-Japanese War/World War II in theBattle of Shanghai, theImperial Japanese Navy launched 45 planes from thefleet aircraft carrierKaga targetingChinese Air Force assets in the province ofJiangsu surrounding Shanghai; thirteenAichi D1A1 dive-bombers were unable to find their intended target inSuzhou and so diverted toJianqiao Airbase instead, but stumbled upon A-12 Shrikes of the26th and 27th Squadrons of the 9th Attack Group at the Chao'er auxiliary airbase preparing for strikes against Japanese positions in Shanghai, and a dogfight ensued between two unlikely dogfighting opponents: two D1A1s were shot down by the Chinese A-12s, and another badly shot-up D1A1 returned toKaga with a fatally wounded crewman.[5]

A-12s served with the3rd Attack Group plus the8th and18th Pursuit Groups. Surviving Shrikes were grounded just afterPearl Harbor wasbombed in December 1941.[6]

Operators

[edit]
An A-12 awaiting delivery to the ROCAF
Republic of China
  • Chinese Nationalist Air Force received 20 A-12 Shrikes in 1936, arming the 27th and the 28th Squadron of the 9th Group. When full-scale war broke out between Japan and China, they were used. They had initial success, including the downing of four JapaneseAichi D1A1carrier-baseddive bombers on 15 August 1937. However, after deploying in ground support missions inShanxi, most did not survive and the few left were reassigned to training duties.[2]
United States

Specifications (A-12 Shrike)

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Data from Curtiss Aircraft 1907–1947,[7] The Complete Encyclopedia of World Aircraft[4]

General characteristics

  • Crew: 2
  • Length: 32 ft 3 in (9.83 m)
  • Wingspan: 44 ft 0 in (13.41 m)
  • Height: 9 ft 0 in (2.74 m)
  • Wing area: 284 sq ft (26.4 m2)
  • Empty weight: 3,898 lb (1,768 kg)
  • Gross weight: 5,756 lb (2,611 kg)
  • Powerplant: ×Wright R-1820-21 Cyclone 9-cylinder air-cooled radial piston engine, 690 hp (510 kW)
  • Propellers: 3-bladed fixed-pitch propeller

Performance

  • Maximum speed: 177 mph (285 km/h, 154 kn)
  • Cruise speed: 150 mph (240 km/h, 130 kn)
  • Range: 520 mi (840 km, 450 nmi)
  • Service ceiling: 15,150 ft (4,620 m)
  • Rate of climb: 1,170 ft/min (5.9 m/s)

Armament

  • Guns:
  • 4 × forward-firing 0.30 in (7.62 mm)M1919 Browning machine guns mounted in the wheel fairings
  • 1 × 0.30 in (7.62 mm) machine gun mounted in the observer's cockpit for rear defense
  • Bombs: Up to 4 × 122 lb (55 kg) bombs carried under the wings[3] or up to 10 × 30 lb (14 kg) fragmentation bombs in fuselage chutes either side of the main fuel tank[6]

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

References

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Notes
  1. ^Fahey, James C.U.S. Army Aircraft 1908–1946. New York: Ships and Aircraft, 1946.
  2. ^abc"Fact Sheet: Curtiss A-12".Museum of the United States Air Force. Archived fromthe original on 5 October 2013. Retrieved7 July 2017.
  3. ^abSwanborough, Gordon; Bowers, Peter M. (1964).United States military aircraft since 1909 (New ed.). New York: Putnam.ISBN 0-85177-816-X.{{cite book}}:ISBN / Date incompatibility (help)
  4. ^abEden and Moeng 2002, p. 514.
  5. ^Cheung, 2015, p. 15.
  6. ^abFitzsimons 1969, p. 2324.
  7. ^Bowers, Peter M. (1979).Curtiss aircraft, 1907–1947. London: Putnam. pp. 327–331.ISBN 0370100298.
Bibliography
  • Eden, Paul and Soph Moeng, eds.The Complete Encyclopedia of World Aircraft. London: Amber Books Ltd., 2002,ISBN 0-7607-3432-1.
  • Fitzsimons, Bernard, ed.The Illustrated Encyclopedia of the 20th Century Weapons and Warfare, Vol. 21. London: Purnell & Sons Ltd., 1969, First edition 1967.ISBN 0-8393-6175-0.
  • Andrade, John M. .U.S Military Aircraft Designations and Serials since 1909. Leicester: Midland Counties Publications, 1979.ISBN 0-904597-22-9.
  • Swanborough, F. G. and Peter M. Bowers.United States Military aircraft since 1909. London: Putnam, 1963, 1971, 1989.ISBN 0-85177-816-X.
  • Bowers, Peter M. .Curtiss Aircraft 1907-1947. London: Putnam, 1979, 1987.ISBN 0-8517-7811-9.
  • Cheung, Raymond.OSPREY AIRCRAFT OF THE ACES 126: Aces of the Republic of China Air Force. Oxford: Bloomsbury Publishing Plc, 2015.ISBN 978 14728 05614.

External links

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