The Dassault Mercure is a twin-engined, narrow-body, jet-powered airliner developed and manufactured by Dassault Aviation, and by Dassault's account the first large-scale European cooperative civil aeronautics programme. It was proposed in 1967 as a French competitor to the Boeing 737 and was the company's first venture into commercial jet airliners, after years of building fighters and executive jets. The French civil aviation directorate had suggested a 140-seat short-haul design, and the programme went ahead with French government backing. The prototype flew on 28 May 1971 and the type entered service on 4 June 1974 with Air Inter. Its range was less than half that of the contemporary Boeing 737-200, which limited its usefulness, and the type sold very poorly: only 12 aircraft were built, between 1971 and 1975, and the last flight was in 1995.
Facts
Engine Class Maximum Mass (kg) Engine2 × Pratt & Whitney JT8D-15 low bypass turbofan engines 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Dassault Mercure (Wikipedia)
Of Make
Source Dassault Mercure (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Dassault Mercure (Wikipedia)LeadQuote, Lead
is a twin-engined narrow-body jet-powered airliner developed and manufactured by French aircraft firm Dassault Aviation
Originated In
Also in Geography Atlas: where this subject originated.
Source Dassault Mercure (Wikipedia)LeadQuote, Lead
is a twin-engined narrow-body jet-powered airliner developed and manufactured by French aircraft firm Dassault Aviation
Sources
1. Dassault Mercure (Wikipedia)
Lead
is a twin-engined narrow-body jet-powered airliner developed and manufactured by French aircraft firm Dassault Aviation
Lead, year
On 28 May 1971, the prototype conducted its maiden flight
Lead, status
The Mercure performed its final flight in 1995.
Specifications
2 × Pratt & Whitney JT8D-15 low bypass turbofan engines
Specifications, mass
Empty weight: 31,800 kg
Specifications, maximum mass
Max takeoff weight: 56,500 kg
Lead, units built
there were only 12 aircraft constructed
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