page_title: Eurofighter Typhoon
section_title: Testing
hierarchical_section_title: Eurofighter Typhoon / Development / Testing
caption_attribution_description: English: Royal Air Force Eurofighter EF-2000 Typhoon F2 (ZJ910) at the 2008 Air Day, Kemble Airport, Gloucestershire, England, showing a deflected canard.
context_page_description: The Eurofighter Typhoon is a twin-engine, canard–delta wing, multirole fighter. The Typhoon was designed originally as an air superiority fighter and is manufactured by a consortium of Airbus, BAE Systems and Leonardo that conducts the majority of the project through a joint holding company, Eurofighter Jagdflugzeug GmbH. NATO Eurofighter and Tornado Management Agency manages the project and is the prime customer.
  The aircraft's development effectively began in 1983 with the Future European Fighter Aircraft programme, a multinational collaboration among the UK, Germany, France, Italy and Spain. Disagreements over design authority and operational requirements led France to leave the consortium to develop the Dassault Rafale independently. A technology demonstration aircraft, the British Aerospace EAP, first flew on 6 August 1986; the first prototype of the finalised Eurofighter made its first flight on 27 March 1994. The aircraft's name, Typhoon, was adopted in September 1998 and the first production contracts were also signed that year.
context_section_description: The maiden flight of the Eurofighter prototype took place in Bavaria on 27 March 1994, flown by DASA chief test pilot Peter Weger. In December 2004, Eurofighter Typhoon IPA4 began three months of Cold Environmental Trials (CET) at the Vidsel Air Base in Sweden, the purpose of which was to verify the operational behaviour of the aircraft and its systems in temperatures between −25 and 31 °C. The maiden flight of Instrumented Production Aircraft 7 (IPA7), the first fully equipped Tranche 2 aircraft, took place from EADS' Manching airfield on 16 January 2008.
caption: Close-up view of RAF Typhoon F2 ZJ910, showing the deflected canard control surface immediately below the pilot
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