2 fatalities

2015-10-03: Piper PA-31-310 Navajo (HK-3909G) — El Caminente Air — Bogotá-Guaymaral, Colombia

Bogotá-Guaymaral, ColombiaTakeoff (climb)

On October 3, 2015, a Piper PA-31-310 Navajo (registration HK-3909G) operated by El Caminente Air was involved in an aviation accident near Bogotá-Guaymaral, Colombia during takeoff. 2 people were killed. Investigators recorded the probable cause as: Failure of the right engine during initial climb due to the failure of internal components. The high density altitude was considered as a contributing factor as it affected the aircraft's performance. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781192757Data APIEditorial standards

Shortly after takeoff from Bogotá-Guaymaral Airport, the pilot declared an emergency due to right engine failure and attempted an emergency landing. The aircraft crashed in a prairie near Los Andes hippodrome, bursting into flames. One passenger was seriously injured; both other occupants were killed.

Accident Summary

Shortly after takeoff from Bogotá-Guaymaral Airport, while climbing, the pilot declared an emergency following the failure of the right engine. The pilot then attempted an emergency landing in an open field. The aircraft subsequently crashed in a prairie located near the Los Andes hippodrome, approximately 5 kilometers northeast of Guaymaral Airport. Upon impact, the aircraft burst into flames.

Emergency and Impact

The emergency was declared after the right engine failed during the initial climb. The pilot's attempt to land in an open field was unsuccessful, resulting in the aircraft crashing in a prairie area. The location of the crash was near the Los Andes hippodrome, about 5 km from the departure airport.

Injuries

A passenger sustained serious injuries, while the other two occupants were killed.

Probable Cause

According to the official investigation, the probable cause of the accident was the failure of the right engine during initial climb due to the failure of internal components. The high density altitude was considered as a contributing factor as it affected the aircraft's performance.