2 fatalities

2017-05-17: Learjet 25 (XA-VMC) — Aerotransportes Huitzilin — Toluca, Mexico

Toluca, MexicoTakeoff (climb)

On May 17, 2017, a Learjet 25 (registration XA-VMC) operated by Aerotransportes Huitzilin was involved in an aviation accident near Toluca, Mexico during takeoff. 2 people were killed. Investigators recorded the probable cause as: Loss of control of the aircraft during the emergency procedure of indication of the deployment of the reverse of the engine number one during the takeoff roll above V1, which was consistent with the training and standard operating procedures that call to… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 1 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781191876Data APIEditorial standards
Aircraft registered XA-VMC
Aircraft registered XA-VMC. Photo: Ojuanialakentu / CC BY-SA 3.0, via Wikimedia Commons

During takeoff on runway 15 at Toluca Airport, a warning light indicated left engine reverse deployment after V1. The crew continued the takeoff per procedures, but during initial climb the aircraft rolled left and crashed, killing both pilots.

Accident Details

On an unspecified date, a multi-engine airplane was conducting a takeoff on runway 15 at Toluca-Licendiado Adolfo López Mateos. During the takeoff roll, after the aircraft passed the V1 speed, a warning light illuminated on the cockpit panel, informing the crew about the deployment of the reverse on the left engine. According to published procedures, the crew continued the takeoff.

Shortly after rotation during the initial climb, the aircraft rolled to the left and crashed in an open field, bursting into flames. The wreckage was located approximately 200 meters past the runway end. The aircraft was destroyed, and both pilots sustained fatal injuries.

Official Findings

The probable cause determined by the investigation was a loss of control of the aircraft during the emergency procedure caused by an indication of the deployment of the reverse on engine number one during the takeoff roll above V1. This was consistent with the training and standard operating procedures that call to continue the takeoff, leading to a collapse of the aircraft due to low speed and abrupt maneuvers and turns toward the engine side in idle position, as well as a commanded opening of the Drag Shut due to poor crew resource management (CRM).

Contributing factors identified include a false indication of the reverse display of the dwelling position number one, and a failure of pilots on previous flights not to report indications of reverse deployment for maintenance actions.