C-GSAT: Air Transat Airbus A310

The Airbus A310 is a wide-body airliner developed and manufactured by Airbus, then a consortium of European aerospace manufacturers. Airbus had demand for an aircraft smaller than the A300, the first Twinjet wide-body. On 7 July 1978, the A310 (initially the A300B10) was launched with orders from Swissair and Lufthansa. On 3 April 1982, the first prototype conducted its maiden flight and it received its type certification on 11 March 1983. Keeping the same eight-abreast cross-section, the A310 is 6.95 m (22.8 ft) shorter than the initial A300 variants, and has a smaller 219 m2 (2,360 sq ft) wing, down from 260 m2 (2,800 sq ft). The A310 introduced a two-crew glass cockpit, later adopted for the A300-600 with a common type rating. It was powered by the same General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofans. It can seat 220 passengers in two classes, or 240 in all-economy, and can fly up to 5,150 nmi (9,540 km). It has overwing exits between the two main front and rear door pairs.