Casualties unknown

Chilean glider crashes into perimeter wall during aborted tow launch

AERÓDROMO “MUNICIPALIDAD DE VITACURA”, CL

On January 6, 2025, a MYD-JS-MD3 was involved in an aviation accident near AERÓDROMO “MUNICIPALIDAD DE VITACURA”, CL. Investigators recorded the probable cause as: An aborted takeoff during a tow launch resulted in the glider veering off the left side of the runway and colliding with a perimeter wall, likely due to loss of control or insufficient stopping distance. 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 2026-09-12Data APIEditorial standards

A MYD JS-MD 3 glider veered off the runway and struck a wall at Vitacura Aerodrome on January 6, 2025. The pilot was uninjured, but the aircraft sustained structural damage.

What happened

On January 6, 2025, at approximately 14:10 local time, a MYD JS-MD 3 glider experienced an incident during a tow launch at the Municipal Aerodrome of Vitacura (SCLC) in Chile's Metropolitan Region. The pilot was attempting to take off from runway 26 while being towed by another aircraft. During the initial phase of the departure, the pilot aborted the takeoff. Instead of stopping on the paved surface, the glider veered off the left side of the runway and collided with a perimeter containment wall and some shrubbery.

The impact caused the aircraft to come to rest outside the runway boundaries, supported by its left wing and the rear section of the tail cone. The pilot, a 69-year-old Chilean national holding a private glider license, was uninjured. However, the investigation noted structural fractures in the forward fuselage skin.

The investigation — what DGAC Chile examined and established

The Directorate General of Civil Aviation (DGAC) initiated a preliminary inquiry under ICAO Annex 13 standards. Investigators reconstructed the flight path from the runway threshold to the final resting position against the wall on the aerodrome's southwest perimeter. They verified that the aircraft was within its weight and balance limits and that all required documentation, including the airworthiness certificate and registration, was valid and present on board.

Meteorological records indicated that conditions were suitable for Visual Meteorological Conditions (VMC) at the time of the event. The DGAC also confirmed that the operator had been performing mandatory maintenance at an authorized center. The aircraft is a 2020 model equipped with a retractable turbine engine for flight assistance, though the incident occurred during a standard tow launch.

Findings

The preliminary evidence points to an aborted takeoff maneuver that resulted in the glider losing directional control or failing to stop within the available runway length. This led to the aircraft leaving the paved surface and impacting the perimeter infrastructure. No mechanical failure was immediately indicated as the primary cause, with the focus remaining on the pilot's decision-making during the abort phase.

Safety action

The investigation is currently in the data collection and analysis phase. The DGAC aims to determine the specific causal factors to issue safety recommendations regarding operational procedures for this type of glider.

Probable cause

An aborted takeoff during a tow launch resulted in the glider veering off the left side of the runway and colliding with a perimeter wall, likely due to loss of control or insufficient stopping distance.

Investigation report by the Chilean Directorate General of Civil Aeronautics (DGAC Chile). Original record: https://www.dgac.gob.cl/informes-2025/. This page is a structured re-presentation; facts and quotes are in the Direccion General de Aeronautica Civil (DGAC), Chile.