Casualties unknown

Incident Involving Piper PA-28 EC-JVQ at Requena Aerodrome

Aeródromo de Requena (Valencia / València), ES

On July 30, 2019, a PIPER PA28-140 (registration EC-JVQ) was involved in an aviation accident near Aeródromo de Requena (Valencia / València), ES. Investigators recorded the probable cause as: The investigation determined that the engine failed because carburetor heat was activated during high ambient temperatures, creating an excessively rich fuel mixture that resulted in insufficient power. 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 2026-09-13Data APIEditorial standards

On July 30, 2019, a Piper PA-28 (EC-JVQ) operated by AIRPULL AVIATION overran the runway at Requena aerodrome after a carburetor heat-induced engine failure. The student pilot was uninjured.

Incident Overview

On July 30, 2019, at approximately 11:15 local time, a Piper PA-28 aircraft with registration EC-JVQ experienced an incident at the Requena aerodrome (LERE) in Valencia, Spain. The aircraft was operated by AIRPULL AVIATION for flight instruction purposes under Visual Flight Rules (VFR). A student pilot was aboard and remained uninjured during the event.

Operational Context

The student pilot had been conducting takeoff and landing exercises on runway 12 since 09:30. Following a landing, the pilot accelerated for another takeoff. At an altitude of approximately 100 feet, the pilot reported that the engine was failing. Consequently, the decision was made to abort the climb and attempt a landing with flaps deployed.

Accident Sequence

Upon touchdown, maximum braking was applied; however, the aircraft could not be stopped within the available runway length. The plane overran the end of the runway, struck the perimeter fence, and came to rest in an adjacent plowed field. The aircraft's longitudinal axis was perpendicular to the runway centerline upon stopping.

Damage and Investigation Findings

The investigation determined that the engine failure was caused by the activation of carburetor heat while ambient temperatures were high (27°C). This condition resulted in an excessively rich fuel mixture, leading to insufficient power. The aircraft sustained minor damage to the landing gear, horizontal stabilizer, and left side of the engine cowling. Additionally, sections of the perimeter fence were damaged or destroyed by the impact.

Probable cause

The investigation determined that the engine failed because carburetor heat was activated during high ambient temperatures, creating an excessively rich fuel mixture that resulted in insufficient power. At the time of failure, there was insufficient remaining runway length to execute a safe landing.