Casualties unknown

Piper PA-36 Suffers Landing Gear Failure After Wheel Strikes Hole During Taxi (EC-EYO)

Puebla del Río (Sevilla), ES

On August 20, 2002, a Piper PA-36-375 (registration EC-EYO) was involved in an aviation accident near Puebla del Río (Sevilla), ES. Investigators recorded the probable cause as: Structural failure of the right main landing gear leg due to an impact load when the wheel entered a hole in the runway, producing a bending moment at the fuselage attachment that caused the leg to fracture. 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 20 August 2002, a Piper PA-36-375 (EC-EYO) broke its right main landing gear leg while taxiing at Las Brujas airstrip in Seville when the wheel entered a hole. The pilot was uninjured; damage was limited to the gear, propeller, and right wing.

Incident Details

On 20 August 2002 at 08:30 local time, a Piper PA-36-375 (registration EC-EYO) was taxiing from the loading area to the runway at Las Brujas airstrip in the municipality of Puebla del Rio, Seville. The aircraft, configured for agricultural aerial application (crop dusting), was executing a left turn when its right main landing gear wheel entered a hole in the taxiway surface. The impact caused the right main gear leg to fracture at its attachment point with the fuselage.

As the leg separated, the aircraft settled onto its right wing, and the propeller contacted the ground. The pilot, a 36-year-old commercial pilot with 3,500 total flight hours, was uninjured.

Damage

Inspection revealed damage to the right main landing gear leg, the propeller, the right wing and flap, and the right boom (pértiga). The aircraft sustained minor damage overall.

Investigation Findings

Visual examination of the failed landing gear leg showed no evidence of material fatigue. The structural failure was attributed to the impact load transmitted through the wheel when it struck the hole. The resulting bending moment at the fuselage attachment exceeded the leg's strength, causing the break. No other contributing factors were identified.

Probable cause

Structural failure of the right main landing gear leg due to an impact load when the wheel entered a hole in the runway, producing a bending moment at the fuselage attachment that caused the leg to fracture.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2002_058_in_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.