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 the world's first short/medium-range jet airliner, produced by the French Sud Aviation firm. Its maiden flight occurred in 1955 when the company was known as SNCASE. The Caravelle was one of the most successful European first-generation jetliners, selling throughout Europe and even penetrating the United States market, with an order for 20 from United Airlines. The Caravelle established the aft-mounted engine, clean-wing design that has since been used on a wide variety of aircraft.
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 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. Various design studies for aircraft in this category had been underway since 1946 by several of the leading French aircraft manufacturing organisations, but none had the financial power to start construction.
Response from the French industry was strong, with every major manufacturer sending in at least one proposal, and a total of 20 different designs were received. Most of the proposals used all-turbojet power, although Breguet entered a number of designs for both turbojet and turboprop types; among these was one for an Atar-powered tri-jet to be developed in association with the SNCA du Nord and a turboprop type, all known as Br. 978. Hurel-Dubois entered several turboprop designs based on a narrow fuselage and shoulder mounted wing similar to many regional propliners. Proposals from the SNCA du Sud-Ouest included the S.O.60 with two Rolls-Royce Avon RA.7 engines, with two smaller Turbomeca Marborés as auxiliaries. SNCA du Sud-Est (SNCASE) returned a number of designs from the X-200 to X-210, all of them pure-jet.