Casualties unknown

Runway excursion during takeoff at Périgueux (F-GMRV)

FR

On August 28, 1998, a BUREAU ENQUETES-ACCIDENTS ACCIDENT survenu à l'avion (registration F-GMRV) was involved in an aviation accident near FR. Investigators recorded the probable cause as: The pilot failed to properly compensate for the effects of the crosswind during the takeoff roll, leading to an asymmetric lift and subsequent loss of directional control. This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA).

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 1786871248Data APIEditorial standards

A Robin DR 400-160 aircraft veered off the runway and sustained heavy damage during takeoff at Périgueux aerodrome.

What happened

On August 28, 1998, at 17:30, a Robin DR 400-160 registered F-GMRV was performing a local flight from Périgueux aerodrome. During the takeoff roll on runway 12, the aircraft's left wing lifted unexpectedly. This caused the right wing to make contact with the runway surface, triggering a 90-degree pivot to the right while the aircraft remained tilted.

The aircraft then exited the runway at high speed, traveling approximately 250 meters. During the excursion, the aircraft struck a signpost, severed three sections of fencing, and broke the nose gear upon hitting an embankment. The aircraft also destroyed a football field barrier before finally coming to a halt after sliding an additional thirteen meters. The aircraft sustained heavy damage.

The investigation

The investigation focused on the flight dynamics during the takeoff roll under the prevailing meteorological conditions. At the time of the accident, the weather was characterized by CAVOK conditions with visibility exceeding 10 km, a temperature of 24 °C, and winds from 060° at 14 knots.

Findings

The investigation established that the primary cause of the runway excursion was the inadequate correction of wind effects by the pilot during the takeoff roll.

Probable cause

The pilot failed to properly compensate for the effects of the crosswind during the takeoff roll, leading to an asymmetric lift and subsequent loss of directional control.