6 fatalities

1995-04-28: Douglas DC-8 (N43UA) — Millon Air — Guatemala City-La Aurora, Guatemala

Guatemala City-La Aurora, GuatemalaLanding (descent or approach)

On April 28, 1995, a Douglas DC-8 (registration N43UA) operated by Millon Air was involved in an aviation accident near Guatemala City-La Aurora, Guatemala during landing or approach. 6 people were killed. Investigators recorded the probable cause as: Wrong approach configuration on part of the crew who landed at an excessive speed of 135 knots in marginal weather conditions. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781208045Data APIEditorial standards
Aircraft registered N43UA
Aircraft registered N43UA. Photo: Pete Macklin / CC BY-SA 2.0, via Wikimedia Commons

A cargo flight operated on behalf of Lineas Aéreas Mayas overran the wet runway at Guatemala City-La Aurora Airport, crashed into houses, killing six people on the ground and injuring all three crew members and seven others on the ground.

Accident

A cargo flight departing Miami International Airport on a route to Lima with an intermediate stop in Guatemala City overran the runway after landing at La Aurora Airport in Guatemala City. The aircraft, operating on behalf of Lineas Aéreas Mayas, touched down on runway 19. Following touchdown, the spoilers were deployed, and reverse thrust was applied on engines number 2 and 3. Due to the wet runway surface, the aircraft could not stop within the remaining distance, overran the runway, went through a fence, and descended an embankment before colliding with several houses.

Injuries

The accident resulted in injuries to all three crew members aboard the aircraft and seven individuals on the ground. Additionally, six other people on the ground were killed.

Probable Cause

The official probable cause of the accident was determined to be a wrong approach configuration on the part of the crew, who landed at an excessive speed of 135 knots in marginal weather conditions. Contributing factors were reported as follows: the runway surface was wet; the braking action was poor; the crew failed to take corrective actions in time; possible aquaplaning occurred; and the crew failed to use all available brake systems.