44 fatalities

1974-06-08: Vickers Viscount (HK-1058) — Aerolineas TAO (Taxi Aéreo Opita) — San Cayetano, Colombia

San Cayetano, ColombiaLanding (descent or approach)

On June 8, 1974, a Vickers Viscount (registration HK-1058) operated by Aerolineas TAO (Taxi Aéreo Opita) was involved in an aviation accident near San Cayetano, Colombia during landing or approach. 44 people were killed. Investigators recorded the probable cause as: Aircraft structure factor – tail unit, involving the failure in flight of the tailplane spar, so that the left tailplane and elevator became detached and control of the aircraft was lost. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781231441Data APIEditorial standards

While descending to Cúcuta-Camilo Daza Airport in good weather, a four-engine airplane lost control and crashed on Mt El Retiro, killing all 44 occupants. The investigation attributed the accident to a fatigue fracture of the left tailplane spar.

Accident Overview

The aircraft was descending to Cúcuta-Camilo Daza Airport at an altitude of 7,000 feet under good weather conditions when it went out of control. It crashed on the slope of Mt El Retiro, located near San Cayetano, approximately 17 kilometers southwest of Cúcuta Airport. The airplane was totally destroyed, and all 44 occupants were killed.

Investigation Findings

Examination of the wreckage revealed that the upper flange of the left tailplane spar had sustained a fatigue fracture. Two distinct areas were visible: the area of progressive fatigue and the area of instantaneous failure. Laboratory tests subsequently confirmed the failure. The already weakened structure was not able to withstand the loads imposed when the aircraft entered an area of turbulence. Weather conditions were considered good and were not considered as a contributing factor.

Probable Cause

Aircraft structure factor – tail unit, involving the failure in flight of the tailplane spar, so that the left tailplane and elevator became detached and control of the aircraft was lost.