Casualties unknown

2001-07-08: Piper PA-38-112 (EC-FPR) — Aeropuerto de Cuatro Vientos (Madrid), ES

Aeropuerto de Cuatro Vientos (Madrid), ES

On July 8, 2001, a Piper PA-38-112 (registration EC-FPR) was involved in an aviation accident near Aeropuerto de Cuatro Vientos (Madrid), ES. Investigators recorded the probable cause as: Hard landing that caused the aircraft to bounce and subsequent loss of control. 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 8 July 2001, a Piper PA-38-112 (registration EC-FPR) veered off the runway after a hard landing during a training flight at Cuatro Vientos Airport (Madrid). The two occupants were uninjured, but the aircraft sustained significant damage.

Accident Overview

On Sunday, 8 July 2001, at 12:50 hours local time, a Piper PA-38-112, registration EC-FPR, operated as a dual-control instructional flight, experienced a runway excursion during landing at Cuatro Vientos Airport in Madrid, Spain. The aircraft had departed from the same airport for a local training flight lasting approximately two hours and fifteen minutes. Upon return, during the landing roll, the aircraft exited the left side of the runway and came to a stop outside the airport perimeter fence.

Aircraft and Crew Information

The aircraft was a single-engine Piper PA-38-112 powered by a Lycoming O-235-L2C engine. The pilot in command was a 28-year-old commercial pilot and instructor with a total of 393 flight hours, including 130 hours on the PA-38 type.

Events Leading to the Accident

According to the instructor's statement, the approach to the airport was performed correctly and in compliance with applicable standards. However, the flare maneuver was executed defectively, causing the aircraft to bounce upon touchdown. The instructor heard the stall warning sound and took control, lowering the nose to gain speed and regain control. The aircraft then bounced a second time and veered left. Observing that the right wing was very close to the ground and believing there was insufficient time to execute a go-around, the instructor decided to continue straight ahead rather than attempt to realign the aircraft with the runway. The aircraft subsequently scraped against the airport perimeter fence and fell to the ground.

Post-Accident Actions

After the aircraft came to rest, the occupants shut off the magnetos and master switch before evacuating the aircraft by their own means. Both occupants were uninjured.

Weather Conditions

Wind data from the METAR at 11:00 UTC indicated intensity of 7 knots from 260°. At the time of the accident, the integrated meteorological system recorded instantaneous wind at 7 knots from 250°, with a 10-minute mean of 5 knots from 250° and a maximum gust of 10 knots.

Damage Assessment

The aircraft sustained significant damage to the propeller, landing gear, and general structure. The airport perimeter fence was also damaged.

Probable Cause

The probable cause of the accident was a hard landing that caused the aircraft to bounce and subsequent loss of control.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2001_037_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.