Accident
Last updated: 2 October 2014
Status:
Datum:Dienstag 31 Oktober 1972
Flugzeugtyp:Silhouette image of generic FA10 model; specific model in this crash may look slightly different
Dassault Falcon 10
Fluggesellschaft:Dassault
Kennzeichen: F-WFAL
Werknummer: 001
Baujahr: 1970-12-01 (1 year 11 months)
Triebwerk: 2 General Electric CJ610-6
Besatzung:Todesopfer: 2 / Insassen: 2
Fluggäste:Todesopfer: 0 / Insassen: 0
Gesamt:Todesopfer: 2 / Insassen: 2
Sachschaden: Zerstört
Konsequenzen: Written off (damaged beyond repair)
Unfallort:Romorantin (   Frankreich) show on map
Flugphase: Manövrieren (MNV)
Betriebsart:Test
Flug von:?
Flug nach:?
Unfallbericht:
First Falcon 10 prototype. The aft fuselage separated as a result of high rudder forces induced at high speed (360kts) at FL150 during runaway rudder trim tests.

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This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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