No fatalities

Cessna 205 EC-GQB Accident in Yeste, Spain

Yeste (Albacete), ES

On March 22, 2014, a Cessna 205 (registration EC-GQB) was involved in an aviation accident near Yeste (Albacete), ES. No fatalities were reported. Investigators recorded the probable cause as: Lack of adequate and effective lubrication in the number 2 crankpin bearing assembly, possibly due to bearing degradation, leading to the fracture of the number 2 connecting rod and complete engine failure. 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
Aircraft registered EC-GQB
Aircraft registered EC-GQB. Photo: Simon Boddy from Maidenhead, Uk / CC BY-SA 2.0, via Wikimedia Commons

On 22 March 2014, a Cessna 205 (EC-GQB) crashed in Yeste, Albacete, after a complete engine failure during cruise. The pilot and passenger sustained minor injuries.

Accident Overview and Flight Details On 22 March 2014, a Cessna 205 with registration EC-GQB departed from the Aeronáutica Delgado maintenance center in Villarrubia, Córdoba, at 16:30 local time. The aircraft was operating a private general aviation flight to its base at Ontur aerodrome in Albacete, where it was dedicated to parachute jumping operations. The flight carried one pilot and one passenger. ## Engine Failure and Emergency Landing Approximately one hour into the flight, while cruising at around 8,000 feet, the engine experienced a sudden loss of power and a drop in oil pressure. The cabin quickly filled with smoke and the smell of burnt oil, prompting the pilot to initiate an emergency landing. The pilot selected a cultivated field in La Donal, within the municipality of Yeste, Albacete. During the landing, the aircraft overturned and came to rest inverted. ## Casualties and Damage Both the pilot and the passenger sustained minor injuries and evacuated the aircraft through a window. The aircraft sustained significant damage, primarily to the left wing and its strut, the vertical stabilizer and rudder, the fuselage behind the cabin, the nose gear, and the propeller. Oil was observed along the lower fuselage beneath the engine. ## Investigation Findings The investigation determined that the accident was caused by a lack of adequate and effective lubrication in the number 2 crankpin bearing assembly, possibly due to bearing degradation. This failure led to the fracture of the number 2 connecting rod and subsequent complete engine failure. The investigation ruled out lubrication system blockages, oil specification non-compliance, and the influence of pre-flight maintenance. A contributing factor was the failure to reduce the time between general overhauls, despite the aircraft's use for parachute jumping and the installation of non-manufacturer engine parts, conditions highlighted in the manufacturer's Service Information Letter SIL 98-9C.

Probable cause

Lack of adequate and effective lubrication in the number 2 crankpin bearing assembly, possibly due to bearing degradation, leading to the fracture of the number 2 connecting rod and complete engine failure.

Investigation report by the Spanish Civil Aviation Accident and Incident Investigation Commission (CIAIAC). Original record: https://www.transportes.gob.es/recursos_mfom/comodin/recursos/2014_006_a.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.