2 fatalities

Cargo Flight 870 Crashes Shortly After Takeoff, Both Pilots Killed (HK-174)

Bogotá-El Dorado, ColombiaTakeoff (climb)

On September 22, 1966, a Douglas DC-4 (registration HK-174) operated by Avianca was involved in an aviation accident near Bogotá-El Dorado, Colombia during takeoff. 2 people were killed. Investigators recorded the probable cause as: Material failure consisting in fatigue failure of a number of teeth of the pinion of the governor control unit, which was jammed against the rack in the 'up' position and therefore set for maximum rpm, thus causing the engine to overspeed. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-12Data APIEditorial standards

A domestic cargo flight from Bogotá to Barranquilla crashed shortly after takeoff, killing both pilots. The aircraft struck trees and was destroyed. Investigation found a governor control failure causing engine overspeed.

Accident Sequence

Flight 870, a scheduled domestic cargo flight from Bogotá-El Dorado International Airport to Barranquilla-Soledad Airport, took off from runway 30 at 0315 hours local time. Witnesses reported the aircraft appeared to lift off with difficulty opposite the control tower. After reaching the airport boundary, the crew announced their intention to return and land. The control tower queried the reason but received no reply. Tower personnel noted that during takeoff, engine noise was louder than usual, as if more than one engine was overspeeding. As the aircraft initiated a turn, a sudden flash was observed, and visual contact was lost. Shortly thereafter, the aircraft struck trees 400 meters from the "San Ramón" property, in a field belonging to the "Laguna Vieja" estate, between the roads leading to Funza and Engativá. The aircraft was destroyed by impact forces and a post-crash fire. Both pilots were killed.

Investigation Findings

The official investigation determined the probable cause to be a material failure: fatigue failure of a number of teeth of the pinion of the governor control unit. This caused the unit to jam against the rack in the "up" position, setting it for maximum rpm and resulting in engine overspeed. This was consistent with the dome ring being at maximum low pitch setting, indicating high rpm and a runaway propeller during takeoff.

A contributing factor was considered to be faulty supervision by the company. The company had briefed the pilot-in-command to conduct a night flight when he was not qualified for DC-4s, as he was still undergoing training for conversion to L-759 aircraft.