Casualties unknown

Piper PA-36-375 Strikes Terrain After Stall During Agricultural Takeoff (EC-EEX)

Puebla del Río (Sevilla), ES

On May 13, 2002, a Piper PA-36-375 (registration EC-EEX) was involved in an aviation accident near Puebla del Río (Sevilla), ES. Investigators recorded the probable cause as: The most probable cause was that the takeoff was performed at a speed close to the aircraft's stall speed, resulting in a stall when a minimal increase in effective angle of attack occurred. 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

A Piper PA-36-375 (EC-EEX) conducting rice seeding crashed on takeoff from Pista de las Brujas, Spain. The pilot, uninjured, had lifted off with insufficient speed, leading to an aerodynamic stall. The aircraft sustained substantial damage.

Introduction

On 13 May 2002, at approximately 11:00 local time, a Piper PA-36-375 (registration EC-EEX) crashed during takeoff from Pista de las Brujas, located in the municipality of Puebla del Río, Seville province. The aircraft was engaged in aerial rice seeding operations, its second flight of the morning.

Accident Details

The accident occurred during the initial climb phase. According to the pilot's statement, during the takeoff roll at the end of the 900-meter runway, the aircraft lifted off with insufficient speed. Consequently, the aircraft stalled and fell into a rice field adjacent to the runway. The pilot shut down the engine upon realizing impact was inevitable, resulting in the engine being stopped at the moment of ground contact.

The aircraft was loaded with 500 kilograms of rice seed and 45 liters of fuel in each wing. Weather conditions were calm wind, temperature 25°C, visibility greater than 10 kilometers, and no clouds.

Damage to the aircraft was substantial, affecting the propeller, landing gear, right wing, fuselage, and engine mount. The pilot was uninjured.

Investigation

Investigators determined that the aircraft had a valid certificate of airworthiness, and the pilot held a valid commercial pilot license with appropriate ratings. No evidence of mechanical failure was found.

A weight and balance calculation, performed according to the aircraft's flight manual, showed that the aircraft's weight and center of gravity were within approved limits and well clear of the boundaries.

Conclusion

The most probable cause of the accident was that the takeoff was performed at a speed close to the aircraft's stall speed, resulting in a stall when a minimal increase in effective angle of attack occurred.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2002_024_a_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.