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Blackburn Lincock

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

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

Design and development Edit

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 Edit

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 Edit

  China
  Japan

Specifications (Lincock III) Edit

 
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

  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.

blackburn, lincock, blackburn, lincock, british, single, seat, lightweight, fighter, produced, blackburn, aircraft, limited, lincock, iirole, single, seat, lightweight, fightermanufacturer, blackburn, aircraft, limitedfirst, flight, 1928number, built, contents. The Blackburn F 2 Lincock was a British single seat lightweight fighter 1 produced by Blackburn Aircraft Limited F 2 LincockBlackburn Lincock IIRole Single seat lightweight fighterManufacturer Blackburn Aircraft LimitedFirst flight 1928Number built 7 Contents 1 Design and development 2 Variants 3 Operators 4 Specifications Lincock III 5 ReferencesDesign and development EditIn 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 EditLincock 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 nbsp Piaggio P 11Operators Edit nbsp ChinaChinese Nationalist Air Force received two aircraft nbsp JapanImperial Japanese Army Air Force received two aircraft Specifications Lincock III Edit nbsp Blackburn Lincock 3 view drawing from l Aerophile April 1931Data from Blackburn Aircraft since 1909 3 General characteristicsCrew 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 propellerPerformance 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 Guns 2 forward firing 303 in 7 7 mm Vickers machine guns 2 References Edit nbsp Wikimedia Commons has media related to Blackburn Lincock Stevens James Hay 22 April 1960 Mirage Flight 558 562 a b Mason 1992 p 204 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 Retrieved from https en wikipedia org w index php title Blackburn Lincock amp oldid 1065827389, wikipedia, wiki, book, books, library,

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