ASN Wikibase Occurrence # 24545
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Thursday 5 August 2004 |
Time: | 11:50 |
Type: | Cessna U206F |
Owner/operator: | Aero Laon Location SARL |
Registration: | F-GPRM |
MSN: | U20602125 |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Destroyed |
Location: | Les Sables-d'Olonne Talmont Airport, Le Château-d'Olonne, Vendee -
France
|
Phase: | Take off |
Nature: | Private |
Departure airport: | Les Sables-d'Olonne Talmont Airport (LSO/LFOO) |
Destination airport: | |
Investigating agency: | BEA |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:According to a rough translation from French Into English of the original BEA France accident report:
"On take-off on runway 07, during the rotation, the pilot finds that the Elevator is blocked. He decides to interrupt the take-off. The The left main landing gear bursts mid-track during braking emergency. Considering that it will not be able to immobilize the aircraft before the end Of the runway, the pilot decides to continue the take-off and
power.
The plane fails to take off, crosses the fence of the airfield, a hedge, A ditch, a field and a road. He finishes his race in a fallow field About one hundred yards from the runway end. When the wreckage is examined, the control cable of the Depth is found broken near its attachment to the compensator.
The metallurgical examination shows that the rupture took place during a Prolonged tension and not under a short and intense effort. Local damage consisting of deep transverse scratches Is at the origin of the rupture (see photographs below). These last Are likely due to inadequate use of a tool during the Positioning of the cable end-piece.
The breaking of the depth compensator control cable caused The positioning of the latter in the full stitched position. It was not possible to To the pilot to counter the aerodynamic effort on the elevator.Under the conditions of the day, the distance necessary for an interruption of Take-off taking into account the flight manual information is About 260 meters"
Aircraft registration F-GPRM struck on: 24/02/2014 for the reason: DESTROYED
Accident investigation:
|
| |
Investigating agency: | BEA |
Report number: | |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
1.
https://www.bea.aero/docspa/2004/f-rm040805/pdf/f-rm040805.pdf 2.
http://web.archive.org/web/20120928112413/http://www.immat.aviation-civile.gouv.fr:80/immat/servlet/aeronef_liste.html;jsessionid=7BA33E88BBA5570CA2F2919DDED4C619 Revision history:
Date/time | Contributor | Updates |
27-Sep-2008 01:00 |
ASN archive |
Added |
21-Dec-2016 23:18 |
Dr. John Smith |
Updated [Time, Operator, Total fatalities, Total occupants, Other fatalities, Phase, Departure airport, Source, Damage, Narrative] |
21-Dec-2016 23:23 |
Dr. John Smith |
Updated [Cn, Operator, Location, Nature, Narrative] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation