Sud Caravelle
| Caravelle | |
|---|---|
 |
|
| Inflight Air France Caravelle III | |
| Role | Narrow-body jet airliner |
| National origin | France |
| Manufacturer | Sud Aviation |
| First flight | 27 May 1955 |
| Introduction | 26 April 1959 with Scandinavian Airlines |
| Retired | 2005 |
| Status | Retired |
| Primary users |
Air France Scandinavian Airlines Swissair Finnair Sabena |
| Produced | 1958–1972 |
| Number built | 282 |
The Sud Aviation SE 210 Caravelle was a French short/medium-range jet airliner. It holds the distinction of being the world's first jet-powered airliner to be developed for the short/medium-range market.
Development of the Caravelle began during the early 1950s under the French aircraft company SNCASE, who were keen to produce a passenger aircraft that utilised newly developed jet propulsion technology. In order to achieve this, SNCASE formed partnerships with British companies such as de Havilland (who provided designs and components which had on their jet-powered airliner, the de Havilland Comet) and Rolls-Royce Limited (from whom the Caravelle's Rolls-Royce Avon turbojet engines were sourced from). While much of the airliner's development, including its maiden flight on 27 May 1955, was conducted under SNCASE; by the time that the Caravelle entered revenue service on 26 April 1959, the firm had been merged into the larger Sud Aviation conglomerate.
Within a few years of commencing passenger services, the Caravelle had become regarded as being one of the most successful European first-generation jetliners. The airliner achieved substantial sales to operators throughout Europe and had even managed to penetrate the United States market, United Airlines placing an order for 20 Caravelles. The Caravelle established the aft-mounted engine, clean-wing design configuration that is still used by smaller jetliners.
On 12 October 1951, the Comité du matériel civil (civil aircraft committee) published a specification for a medium-range aircraft, which was later sent to the aviation industry by the Direction technique et industrielle. This called for an aircraft capable of carrying 55 to 65 passengers and 1,000 kg (2,200 lb) of cargo on routes up to 2,000 km (1,100 nmi; 1,200 mi) with a cruising speed of about 600 km/h (320 kn; 370 mph). The type and number of engines were not specified. Since 1946, various design studies for aircraft in this category had already been underway at several of the leading French aircraft manufacturing organisations, and had resulted in some ambitious concepts being mooted. However, none of these firms possessed the financial power to independently embark on the substantial development work involved, let alone to establish a manufacturing line for the construction of such aircraft.
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