Accident
Last updated: 19 May 2013
| Status: | |
| Datum: | 31 OKT 1972 |
| Flugzeugtyp: | 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)
 |
| Flugphase: | Manövrieren (MNV) |
| Betriebsart: | Test |
| Flug von: | ? |
| ? |
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.
Informationsquelle:
Fotos
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.
