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Gloster Gannet

General Aviation and Light Aircraft

The Gloster Gannet was a tiny single-seat, single-engined biplane built by the Gloucestershire Aircraft Company at Cheltenham for the light aircraft trials held at Lympne in 1923, where engine size was limited to 750 cc to encourage cheap private flying. It was among the smallest aircraft built in Britain and had wings that folded back along the fuselage for easy storage. Its specially designed Carden two-cylinder two-stroke engine overheated and lacked lubrication, so it could not fly in the contest although it was present as G-EBHU. It was later re-engined with a seven horsepower Blackburne Tomtit and was scrapped in 1932.

Facts
Year
1923 1
Top Speed (km/h)
120 1
Mass (kg)
150 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Gloster Gannet (Wikipedia)

Of Make

Source Gloster Gannet (Wikipedia)
Sources
1. Gloster Gannet (Wikipedia)
  • Lead, built for the 1923 Lympne trials
    built by the Gloucestershire Aircraft Company Limited of Cheltenham, United Kingdom, to compete in the 1923 Lympne Trials
  • Lead, aircraft
    single-seat single-engined light aircraft
  • Specifications, maximum speed
    Maximum speed: 72 mph (115 km/h, 63 kn)
  • Specifications, empty weight
    Empty weight: 330 lb (149 kg)
  • Lead and development, maker
    The Gannet was Gloster's intended entry.
  • Lead, British aircraft
    built by the Gloucestershire Aircraft Company Limited of Cheltenham, United Kingdom
  • In Group: Single-Engine Piston Light Aircraft, Lead, aircraft role
    single-seat single-engined light aircraft
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