Casualties unknown

2002-08-13: Socata TB-10 Tobago (EC-FSN) — Aeropuerto de Salamanca (Salamanca), ES

Aeropuerto de Salamanca (Salamanca), ES

On August 13, 2002, a Socata TB-10 Tobago (registration EC-FSN) was involved in an aviation accident near Aeropuerto de Salamanca (Salamanca), ES. Investigators recorded the probable cause as: The cause of the incident was the incorrect execution of the landing maneuver. 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 13 August 2002, a SOCATA TB10 (EC-FSN) conducting a solo student flight bounced multiple times during landing at Salamanca Airport, causing substantial damage to the landing gear and airframe. The student pilot reported misjudging the approach.

Event Summary

On 13 August 2002 at 13:15 local time, a SOCATA TB10 (registration EC-FSN) sustained damage during a landing at Salamanca Airport. The aircraft, a single-engine 1993 model powered by a Textron Lycoming O-360-AIAD engine, was engaged in a solo training flight as part of a student pilot's private pilot license course. The student pilot, aged 21 with 50 flight hours, had taken off for a local area flight. Weather conditions were good with no clouds and wind at 4 knots.

Pilot Report

According to the student pilot's statement, during the approach she noticed she was higher than expected on final and, lacking wind, decided to extend full flaps and glide. After conducting an initial flare, she performed a second flare but found herself with insufficient altitude to complete it, resulting in the aircraft touching down on all three wheels. The airplane then bounced at least twice. She responded by adding power and executed a successful landing without further event.

Aircraft Examination

Post-incident inspection revealed damage primarily to the landing gear. Further examination in a workshop, after removal of the engine and propeller, showed that the engine mount was bent, causing deformation of the firewall. Upon removal of the firewall, it was discovered that fuselage station zero and the upper fuselage panel were also damaged.

Conclusion

The investigation concluded that the cause of the incident was the incorrect execution of the landing maneuver.

Probable cause

The cause of the incident was the incorrect execution of the landing maneuver.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/2002_055_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.