Casualties unknown

Loss of Control During Landing Roll Involving Piper PA-36-285 (EC-CQU)

Villafranco del Guadalquivir (Sevilla), ES

On June 14, 2000, a Piper PA-36-285 (registration EC-CQU) was involved in an aviation accident near Villafranco del Guadalquivir (Sevilla), ES. Investigators recorded the probable cause as: The incident was caused by a probable combination of a strong gust of wind (main factor) and the narrow width of the runway (contributing factor). This summary draws on records from the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC).

Sourcesthe Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC)Primary reportUpdated 2026-09-13Data APIEditorial standards

On 14 June 2000, a Piper PA-36-285 (EC-CQU) conducting aerial application lost directional control during landing roll at Villafranco del Guadalquivir due to a wind gust, exiting the runway into an adjacent canal. Pilot uninjured.

Aircraft and Pilot Information

The aircraft involved was a Piper PA-36-285, serial number EC-CQU, manufactured in 1975. It was equipped with a single Lycoming O-540-K1G5 engine. The pilot, aged 42, held a commercial pilot license and had accumulated 2,409 total flight hours. The operation was classified as general aviation commercial aerial application.

Accident Narrative

On 14 June 2000 at 13:20 local time, the aircraft had completed an aerial treatment flight and proceeded to the temporary runway at Villafranco del Guadalquivir in the province of Seville for landing. The approach and touchdown were normal. During the subsequent landing roll, according to the pilot's statement, a gust of wind pushed the aircraft to the right. The pilot lost directional control, and the aircraft exited the runway, ultimately falling into a canal that runs adjacent and parallel to the runway.

Injuries and Damage

The pilot, the sole occupant of the aircraft, was uninjured. The aircraft sustained substantial damage.

Weather Conditions

Meteorological conditions at the time included variable wind from the east-west direction, visibility greater than 10 kilometers, no clouds, and a temperature of 25°C.

Investigation Analysis

The investigation determined that the loss of directional control was probably caused by a strong gust of wind from the right side of the aircraft, causing it to deviate to the right. The pilot was unable to regain control. Additionally, temporary runways such as the one used often have a narrower width than permanent aerodromes, and in this case, the right edge of the runway was bordered by a canal. The incident was attributed to a probable combination of two factors: the wind gust (main factor) and the narrow width of the runway (contributing factor).

Probable cause

The incident was caused by a probable combination of a strong gust of wind (main factor) and the narrow width of the runway (contributing factor).

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2000_015_in_bis_0.pdf. This page is a structured re-presentation; facts and quotes are in the Comision de Investigacion de Accidentes e Incidentes de Aviacion Civil (CIAIAC), Spain - Ministerio de Transportes y Movilidad Sostenible.