Blackburn Lincock

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F.2 Lincock
Blackburn Lincock II ExCC.jpg
Blackburn Lincock II
Role Single-seat lightweight fighter
Manufacturer Blackburn Aircraft Limited
First flight 1928
Number built 7

The Blackburn F.2 Lincock was a British single-seat lightweight fighter[1] produced by Blackburn Aircraft Limited.

Design and development[]

In 1928 Blackburn designed and built a private venture lightweight biplane fighter powered by an Armstrong Siddeley Lynx IVC engine. The Blackburn F.2 Lincock was of wooden construction and first appeared in May 1928. It performed well in demonstrations but failed to gain any orders. The Canadian government showed an interest in the design, and a metal construction variant (the Lincock II) was built. It was tested in Canada at Camp Borden in 1930 where there was interest in using the Lincock as an advanced 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 the Lincock III of which five were produced, two were delivered to China, two to Japan and one retained as a demonstrator. Interest from Italy resulted in Piaggio acquiring a licence to produce a two-seat version as an aerobatic trainer, though only one Piaggio P.11 was built.

Variants[]

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 in Italy.
Piaggio P.11

Operators[]

 China
  • Chinese Nationalist Air Force received two aircraft.
 Japan
  • Imperial Japanese Army Air Force received two aircraft.

Specifications (Lincock III)[]

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[]

  1. ^ Stevens, James Hay (22 April 1960), "Mirage", Flight: 558–562
  2. ^ a b Mason 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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