Casualties unknown

2003-09-13: Piper PA-31 (EC-CDS) — Aeropuerto de Barcelona (Barcelona), ES

Aeropuerto de Barcelona (Barcelona), ES

On September 13, 2003, a Piper PA-31 (registration EC-CDS) was involved in an aviation accident near Aeropuerto de Barcelona (Barcelona), ES. Investigators recorded the probable cause as: The nose gear failed to complete its extension sequence before making contact with the runway, likely due to the nose tire being underinflated, which caused the tire to rotate and shear the valve. This summary draws on records from the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC)Primary reportUpdated 1785075856Data APIEditorial standards

A Piper PA-21 experienced a nose gear collapse during its landing roll at Barcelona Airport, resulting in significant damage to the aircraft but no injuries to the crew.

What happened

On September 13, 2003, at approximately 03:15, a PIPER PA-21, registration EC-CDS, was performing a positioning flight from Palma de Mallorca to Barcelona Airport. The aircraft, operated by Tadair, S. A., was being piloted by a co-pilot with approximately 100 hours of experience in the type.

During the landing roll on runway 02, the aircraft suffered a nose gear collapse shortly before reaching the intersection of the airport's two runways. The impact caused the aircraft to come to a stop on its main gear and the nose gear doors. The two crew members on board were uninjured and were able to evacuate the aircraft without difficulty.

The investigation

The investigation focused on the mechanical state of the landing gear and the circumstances of the impact. Inspections of the wreckage revealed that the main landing gear was locked in the down position. During the recovery process, the nose gear was observed to drop and lock correctly.

Investigators found that the nose tire was deflated and had rotated approximately one-third of a revolution on the rim, which had caused the valve to be sheared. There were no signs of a puncture or high-speed contact with the runway on the tire itself. Additionally, the left main gear strut was found to be collapsed, having lost its hydraulic fluid and air pressure due to damaged internal O-rings.

Ground functional tests performed on the aircraft while on jacks showed that the landing gear operated correctly, with all three legs locking securely in the extended position. Maintenance records indicated that the strut had been serviced 15 days prior to the incident with no anomalies noted.

Probable cause

The nose gear failed to complete its extension sequence before making contact with the runway, likely due to the nose tire being underinflated, which caused the tire to rotate and shear the valve.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2003_058_in.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.