Casualties unknown

2017-06-10: Piper PA-28-151 (EC-HPN) — Aeródromo de Casarrubios del Monte (Toledo), ES

Aeródromo de Casarrubios del Monte (Toledo), ES

On June 10, 2017, a Piper PA-28-151 (registration EC-HPN) was involved in an aviation accident near Aeródromo de Casarrubios del Monte (Toledo), ES. Investigators recorded the probable cause as: The runway excursion originated from a very advanced touchdown that, combined with the crew's stress, aggravated the landing. 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 1785075856Data APIEditorial standards

On 10 June 2017, a Piper PA-28-151 (EC-HPN) on an instructional flight suffered a runway excursion during landing at Casarrubios del Monte Aerodrome. The crew reported aileron control, vertical speed indicator, and brake failures. Investigation found no technical faults; both occupants were uninjured.

Flight Details

On 10 June 2017, at 15:10 local time, a Piper PA-28-151, registration EC-HPN, was involved in a runway excursion during landing on runway 08 at Casarrubios del Monte Aerodrome (Toledo, Spain). The aircraft was operated by the flight school Airpilot (Flyschool) and was conducting a dual instruction flight as part of a private pilot license course. On board were an instructor and a student pilot, both uninjured. The flight originated from Cuatro Vientos Airport (Madrid) approximately 21 minutes earlier, with the intention of performing basic flight maneuvers under visual flight rules.

Reported Failures

During the flight, about 13 minutes after departure, the aircraft experienced a left bank of 40–50° with resistance in the flight controls. The crew identified a possible aileron control failure. After leveling the aircraft, they diverted to Casarrubios del Monte. During approach and descent, a second failure was reported involving the vertical speed indicator. During the landing roll on runway 08, a third failure occurred, described as a brake locking.

Investigation Findings

The investigation examined the flight control system, vertical speed indicator, and braking system. No technical faults were found in any of these systems. The reported aileron and vertical speed indicator issues were attributed to probable turbulence. The runway excursion was determined to have resulted from a very advanced touchdown on the runway, leaving insufficient remaining distance for braking, compounded by the crew’s stress from believing they were flying an aircraft with a control failure.

Conclusions

The probable cause of the incident was a very advanced touchdown that, combined with the crew’s stress, aggravated the landing and led to the runway excursion. No further contributing factors were identified. The investigation also noted three administrative issues (failure to report the incident, ELT status, and lack of traceability of an aileron servo) that were addressed by the involved organizations, and no safety recommendations were issued.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2017_008_in_new.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.