No fatalities

Landing Gear Failure During Training Flight at Cuatro Vientos (EC-HYP)

Aeropuerto de Cuatro Vientos (Madrid), ES

On August 31, 2003, a Piper PA-34 Seneca (registration EC-HYP) operated by Private was involved in an aviation accident near Aeropuerto de Cuatro Vientos (Madrid), ES. No fatalities were reported. Investigators recorded the probable cause as: Fatigue and stress corrosion cracking of the right main landing gear trunnion, leading to a static overload failure during the landing roll. 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 2026-10-18Data APIEditorial standards

A Piper PA-34-200T (EC-HYP) suffered a right main landing gear failure during a training flight at Cuatro Vientos Airport on August 31, 2003. The aircraft dragged on the runway, but all three occupants escaped without injury.

Incident Overview and Flight Details On August 31, 2003, a Piper PA-34-200T, registration EC-HYP, operated by Aerea Flying Training Organization, departed from runway 28 at Cuatro Vientos Airport in Madrid at approximately 09:05 local time. The aircraft was conducting a general aviation training flight with dual command. The flight crew consisted of a 32-year-old commercial pilot acting as the pilot in command and instructor, a commercial pilot undergoing training for a license renewal, and a second instructor seated in the rear. The aircraft was fully fueled and completed a series of normal training maneuvers before returning to the airport. The approach to runway 28 was uneventful, with a headwind of approximately 5 knots. The landing gear was lowered and locked, indicated by three green lights in the cockpit. The aircraft was cleared to land at 09:51 and touched down in the first third of the runway. Occupants described the landing as normal, though slightly hard, with the wings level. During the landing roll, the instructor took control of the aircraft. As speed decreased, the right wing began to lower progressively. The instructor applied left aileron, but the right landing gear leg eventually failed, causing the aircraft to rest on the right side of the runway. The aircraft came to a stop approximately 980 meters from the start of runway 28, having dragged for about 500 meters, primarily on the right wheel and the cabin access step. The right wingtip was approximately one meter from the runway edge. The occupants, who were uninjured, shut down the engines and electrical systems and evacuated the aircraft. The runway was closed from 09:52 to 10:45 while fire crews removed the aircraft. No fire occurred, although there was a risk due to fuel and hydraulic fluid leaks and sparks from the drag. Debris, including parts of the shock absorber piston and brake pads, was recovered from the runway.

Probable cause

Fatigue and stress corrosion cracking of the right main landing gear trunnion, leading to a static overload failure during the landing roll.

Frequently asked questions

What happened in the 31 Aug 2003 Piper PA-34 Seneca accident near Aeropuerto de Cuatro Vientos (Madrid), ES?

A Piper PA-34-200T (EC-HYP) suffered a right main landing gear failure during a training flight at Cuatro Vientos Airport on August 31, 2003. The aircraft dragged on the runway, but all three occupants escaped without injury.

Were there any fatalities in the 31 Aug 2003 Piper PA-34 Seneca accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 31 Aug 2003 involved a Piper PA-34 Seneca, registration EC-HYP, operated by Private, at Aeropuerto de Cuatro Vientos (Madrid), ES.

What was the probable cause of the accident?

Fatigue and stress corrosion cracking of the right main landing gear trunnion, leading to a static overload failure during the landing roll.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2003_052_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.