Casualties unknown

2019-01-18: Bristell N65 (CC-AUV) — Aeródromo “Eulogio Sánchez”, CL

Aeródromo “Eulogio Sánchez”, CL

On January 18, 2019, a Bristell N65 (registration CC-AUV) was involved in an aviation accident near Aeródromo “Eulogio Sánchez”, CL. Investigators recorded the probable cause as: Loss of control in flight during a turn to return to the runway, as a result of engine stoppage during initial climb. The technical reason for the engine stoppage could not be determined due to the level of damage to the external components of the engine. This summary draws on records from the Chilean Directorate General of Civil Aeronautics (DGAC Chile).

Sourcesthe Chilean Directorate General of Civil Aeronautics (DGAC Chile)Primary reportUpdated 1785022237Data APIEditorial standards

The Chilean DGAC closed the investigation into the 18 January 2019 accident of a Bristell S-LSA (CC-AUV) at Aeródromo Eulogio Sánchez. The instructor died and the student was seriously injured. The probe was reopened after a report that the aircraft took off with the Gascolator drain valve open.

Accident

On 18 January 2019 at 09:03 local time, a BRM Aero S.R.O. Bristell S-LSA, registration CC-AUV, crashed during initial climb after takeoff from Aeródromo Eulogio Sánchez (SCTB) in La Reina, Metropolitan Region. The aircraft experienced an engine stoppage, subsequently lost control during a turn to return to the runway, impacted terrain, and caught fire. The pilot instructor, Nicolás Osorio Larrosa, was fatally injured; the student pilot, Cristóbal Arriagada Muñoz, sustained serious injuries.

Initial Investigation

Investigación N°1882WS was opened by the Dirección General de Aeronáutica Civil (DGAC) on 21 January 2019. The initial closure, by Resolution Exenta N°1013 on 9 October 2019, determined the probable cause as "loss of control in flight during a turn to return to the runway, as a result of engine stoppage during initial climb." The technical reason for the engine stoppage could not be determined due to the extent of damage to external engine components.

Reopening

On 11 March 2020, the DGAC's Departamento de Seguridad Operacional reported a new technical antecedent: the aircraft had taken off with the Gascolator drain valve open. Based on this, Resolution Exenta N°1163 of 30 October 2020 revoked the earlier closure and ordered the investigation reopened to examine this possible cause. The manufacturer of the engine (Rotech Flight Safety – Rotax Aircraft Engines, Canada) had previously examined the wreckage and found no internal mechanical anomalies, but the open valve could have led to fuel starvation.

Final Closure

The reopened investigation concluded with Resolution Exenta N°2346 on 30 October 2025. The final closure acknowledged the new antecedent but did not revise the probable cause; the technical analysis from 6 January 2022 considered the open drain valve. The DGAC closed the case without explicitly restating the cause, though the original determination remains on record.

Investigation report by the Chilean Directorate General of Civil Aeronautics (DGAC Chile). Original record: https://www.dgac.gob.cl/informes-2019/. This page is a structured re-presentation; facts and quotes are in the Direccion General de Aeronautica Civil (DGAC), Chile.