Fatigue-induced landing gear failure causes runway excursion at Igualada Aerodrome

Casualties unknown • Aeródromo de Igualada (Barcelona), ES

A Piper PA-23-250 experienced a left main landing gear collapse during landing, resulting in a runway excursion and minor aircraft damage.

What happened

On June 9, 2012, a PIPER PA-23-250 Aztec E, registration EC-GGF, was performing a private flight from Sabadell Airport to Igualada Aerodrome when the aircraft suffered a runway excursion. During the landing roll on runway 17, the pilot noticed the left main landing gear was giving way. The aircraft traveled approximately 330 meters before coming to a stop, having veered off the runway to the left. The aircraft eventually rested on its nose gear, right main gear, and left wing. All six occupants—the pilot and five passengers—were uninjured.

The investigation

The CIAIAC investigation focused on the structural integrity of the landing gear and the maintenance history of the aircraft. Investigators examined the wreckage, noting that the left main gear strut had cracked, causing the drag link attachment projection to separate from the strut. Laboratory analysis of the fractures confirmed that the failure originated from a fatigue process in the area where the main gear drag link attaches to the strut.

While eyewitnesses described the landing as very hard, investigators determined that such an impact, if it occurred, only accelerated the failure of an already compromised component. The investigation also reviewed the aircraft's maintenance records, noting that the gear had been in service for 40 years, with the last 15 years involving high-demand training operations. The maintenance program, which followed manufacturer specifications, relied on flight hours rather than landing cycles and did not include specific inspections or overha-uls for the gear components involved.

Probable cause

The left main landing gear failed due to fatigue cracking in the strut projection, a defect that was invisible to the naked eye and undetectable through standard visual inspections. This fatigue was driven by the high number of landing cycles and the long-term operational life of the component, exacerbated by the lack of cycle-based maintenance or specialized non-destructive testing requirements.

Frequently asked questions

What happened in the 2012-06-09 Piper PA-23-250 accident near Aeródromo de Igualada (Barcelona), ES?

A Piper PA-23-250 experienced a left main landing gear collapse during landing, resulting in a runway excursion and minor aircraft damage.

What aircraft was involved and where did it happen?

The accident on 2012-06-09 involved a Piper PA-23-250, registration EC-GGF, at Aeródromo de Igualada (Barcelona), ES.

What was the probable cause of the accident?

The left main landing gear failed due to fatigue cracking in the strut projection, a defect that was invisible to the naked eye and undetectable through standard visual inspections. This fatigue was driven by the high number of landing cycles and the long-term operational life of the component, exacerbated by the…

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2012_020_in_eng_2.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.

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