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Blackburn Lincock

From Wikipedia, the free encyclopedia

F.2 Lincock
Blackburn Lincock II
General information
TypeSingle-seat lightweight fighter
ManufacturerBlackburn Aircraft Limited
Number built7
History
First flight1928

TheBlackburn F.2 Lincock was a British single-seatlightweight fighter[1] produced byBlackburn Aircraft Limited.

Design and development

[edit]

In 1928 Blackburn designed and built a private venture lightweightbiplane fighter powered by anArmstrong Siddeley Lynx IVC engine. TheBlackburn F.2 Lincock was of wooden construction and first appeared in May 1928. It performed well in demonstrations but failed to gain any orders. TheCanadian government showed an interest in the design, and a metal construction variant (theLincock II) was built. It was tested in Canada at Camp Borden in 1930 where there was interest in using the Lincock as anadvanced trainer, but the type was not ordered.[2] It was later used to perform public aerobatic displays in 1933 and 1934.

The final version was theLincock III of which five were produced, two were delivered to China, two to Japan and one retained as a demonstrator. Interest from Italy resulted inPiaggio acquiring a licence to produce a two-seat version as an aerobatic trainer, though only onePiaggio P.11 was built.

Variants

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Lincock I
Wooden-construction prototype, one built.
Lincock II
Metal-construction prototype, one built.
Lincock III
Production version, five built.
Piaggio P.11
two-seat aerobatic trainer, one built inItaly.
Piaggio P.11

Operators

[edit]
 China
 Japan

Specifications (Lincock III)

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Blackburn Lincock 3-view drawing from l'Aerophile April 1931

Data from Blackburn Aircraft since 1909[3]

General characteristics

  • Crew: 1
  • Length: 19 ft 6 in (5.94 m)
  • Wingspan: 22 ft 6 in (6.86 m)
  • Height: 7 ft 4 in (2.24 m)
  • Wing area: 170 sq ft (16 m2)
  • Empty weight: 1,326 lb (601 kg)
  • Max takeoff weight: 2,082 lb (944 kg)
  • Powerplant: 1 ×Armstrong Siddeley Lynx Major 7-cylinder air-cooled radial pistone engine, 270 hp (200 kW)
  • Propellers: 2-bladed fixed-pitch propeller

Performance

  • Maximum speed: 164 mph (264 km/h, 143 kn) at sea level
  • Range: 380 mi (610 km, 330 nmi)
  • Service ceiling: 23,000 ft (7,000 m)
  • Rate of climb: 1,660 ft/min (8.4 m/s)

Armament

References

[edit]
Wikimedia Commons has media related toBlackburn Lincock.
  1. ^Stevens, James Hay (22 April 1960),"Mirage",Flight:558–562
  2. ^abMason 1992, p. 204.
  3. ^Jackson 1968, pp. 267–268.
  • Jackson, A.J. (1968).Blackburn Aircraft since 1909. London: Putnam.ISBN 0-370-00053-6.
  • Mason, Francis K (1992).The British Fighter since 1912. Naval Institute Press.ISBN 1-55750-082-7.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
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