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The Pilots Desk
AirlinersBritish-French supersonic airliner (1969–2003)

Concorde

Concorde

Concorde ( KONG-kord, French: [kɔ̃kɔʁd] ) is a retired Anglo-French supersonic airliner jointly developed and manufactured by Sud Aviation and the British Aircraft Corporation (BAC). Studies began in 1954 and a UK–France treaty followed in 1962, as the programme cost was estimated at £70 million (£1.77 billion in 2025). Construction of six prototypes began in February 1965, with the first flight from Toulouse on 2 March 1969. The market forecast was 350 aircraft, with manufacturers receiving up to 100 options from major airlines. On 9 October 1975, it received its French certificate of airworthiness, and was certified by the UK CAA on 5 December. Concorde is an aircraft design with a narrow fuselage permitting four-abreast seating for 92 to 128 passengers, an ogival delta wing, and a droop nose for landing visibility. It is powered by four Rolls-Royce/Snecma Olympus 593 turbojets with variable engine intake ramps, and reheat for take-off and acceleration to supersonic speed. Constructed from aluminium, it was the first airliner to have analogue fly-by-wire flight controls. The airliner had transatlantic range while supercruising at twice the speed of sound for 75% of the distance. Delays and cost overruns pushed costs to £1.5–2.1 billion in 1976 (£12–16.7 billion in 2025). Concorde entered service on 21 January 1976 with Air France from Paris-Roissy and British Airways from London Heathrow. Transatlantic flights were the main market, to Washington Dulles from 24 May, and to New York JFK from 17 October 1977. Air France and British Airways remained the sole customers with seven airframes each, for a total production of 20. Supersonic flight more than halved travel times, but sonic booms over the ground limited it to transoceanic flights only. Its only competitor was the Tupolev Tu-144, carrying passengers from November 1977 until a May 1978 crash, while a potential competitor, the Boeing 2707, was cancelled in 1971 before any prototypes were built. On 25 July 2000,

Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.

Manufacturer
Sud-Aviation
Category
Airliners
First flight
1969-03-02
Length
61.66 m
Wingspan
25.56 m

Specifications

Cruise speed
1,165 kt
Max speed
1,177 kt
Range
3,900 nm
Service ceiling
60,000 ft
Rate of climb
5,000 ft/min
Max takeoff weight
408,010 lb
Empty weight
173,504 lb
Fuel capacity
31,600 US gal
Powerplant
Rolls-Royce/Snecma Olympus 593
Engines
4
Seats
128
Length
202.3 ft
Wingspan
84 ft
Height
40 ft
Number built
20

Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).

Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.