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The Fairey Fox was a British light bomber and fighter biplane of the 1920s and 1930s. It was originally produced in Britain for the RAF, but continued in production and use in Belgium long after it was retired in Britain.

Development and design

Fox I

In 1923, Charles Richard Fairey, founder and chief designer of Fairey Aviation, disappointed with his Fawn bomber, which owing to the constraints of Air Ministry specifications, was slower than the Airco DH.9A which it was meant to replace while carrying no greater bombload, conceived the idea of a private venture bomber not subject to official limitations, which could demonstrate superior performance and handling. On seeing the Curtiss CR, powered by a Curtiss D-12 V-12 liquid-cooled engine of low frontal area and in a low drag installation, win the 1923 Schneider Trophy race, Fairey realised that this engine would be well suited to a new bomber and acquired an example of the engine and a licence for production.

Fairey began design of a bomber around this engine, with detailed design carried out by a team at first led by Frank Duncanson and then by the Belgian Marcel Lobelle. The resultant aircraft, the Fairey Fox, was a single-bay biplane with highly staggered wings, The Curtiss D-12 was installed in a closely cowled tractor installation, with one radiator mounted on the underside of the upper wing, and a second retractable radiator that could be wound in and out of the fuselage as required. Up to of bombs could be carried under the wings, aimed by the gunner whose seat folded to allow use of a bombsight. Despite this, there was much resistance to the new bomber within the Air Ministry, with the Fox not designed to an official specification and having several features, such as fuel tanks within the fuselage, that went against official norm, and most importantly, it featured an American engine.