The Dassault Falcon 30 was a prototype French jet regional airliner of the 1970s, developed by Dassault Aviation from the Falcon 20 business jet and made larger, with more powerful engines and room for about 40 passengers. Earlier proposals, the Mystère 30 of 1963 and the Falcon 20T of 1970, stalled for lack of a suitable engine; work restarted when the Avco Lycoming ALF 502 geared turbofan became available, which led to a longer forward fuselage, a new wing centre-section and a larger tail. The single prototype was completed in March 1973 and first flew on 11 May 1973 at Mérignac, then appeared at the Paris Air Show. No production followed. The prototype was later broken up, with its fuselage going to a technical school and then to an aviation museum in Aquitaine.
Facts
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Dassault Falcon 30 (Wikipedia)
Of Make
Source Dassault Falcon 30 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Dassault Falcon 30 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
It was developed by Dassault Aviation from its successful Falcon 20 business jet
Originated In
Also in Geography Atlas: where this subject originated.
Source Dassault Falcon 30 (Wikipedia)Lead, country of originQuote, Lead, country of origin
was a prototype French jet-powered regional airliner of the 1970s
Sources
1. Dassault Falcon 30 (Wikipedia)
Lead
flying for the first time on 11 May 1973
Specifications
2 × Lycoming ALF 502D turbofan
Lead, body style
was a prototype French jet-powered regional airliner
Lead, status
A single prototype was built
Specifications, mass
Empty weight: 10,050 kg
Specifications, maximum mass
Max takeoff weight: 16,000 kg
Lead, manufacturer
It was developed by Dassault Aviation from its successful Falcon 20 business jet
Lead, country of origin
was a prototype French jet-powered regional airliner of the 1970s
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