71 fatalities

Night Approach Accident at Douala Airport (TJ-CBE)

Douala, CameroonLanding (descent or approach)

On December 3, 1995, a Boeing 737-200 (registration TJ-CBE) operated by Cameroon Airlines was involved in an aviation accident near Douala, Cameroon during landing or approach. 71 people were killed. Investigators recorded the probable cause as: The accident resulted from a loss of control of the aircraft during an attempted go-around made during the touchdown maneuver on landing, with degraded performance. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 5 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards
Boeing 737-200
Photo: San Diego Air & Space Museum Archives / Public domain, via Wikimedia Commons

An aircraft crashed into a mangrove near Douala Airport during a night approach after a go-around attempt, killing 71 occupants and injuring five.

Incident Overview During a night approach to Douala Airport, the crew received clearance to land on runway 30 at a distance of 3.5 nautical miles. The aircraft then initiated a slight climb, and approximately 15 seconds later, the copilot reported technical problems to air traffic control. Three seconds after that report, the aircraft rolled to the left, struck trees, and crashed into a mangrove located about 1,700 metres south of runway 30. The aircraft burst into flames upon impact. ## Casualties The accident resulted in 71 fatalities among the occupants. Three passengers and two crew members, identified as the copilot and a stewardess, were seriously injured. ## Official Findings The official investigation determined that the accident resulted from a loss of control during an attempted go-around made during the touchdown maneuver on landing, with degraded performance. Contributing factors included the detachment by structural fatigue of a blade from the first stage of the compressor on engine number 1, which led to a loss of power. Additionally, the trajectory was destabilized during landing, and the go-around procedure was executed late or slowly in an unidentified single-engine configuration, resulting in an irreversible loss of speed.

Probable cause

The accident resulted from a loss of control of the aircraft during an attempted go-around made during the touchdown maneuver on landing, with degraded performance. Contributing factors were the detachment by structural fatigue of a blade from the first stage of the compressor on engine number 1, leading to a loss of power, and a destabilization of the trajectory during landing with a late or slow execution of the go-around procedure in an unidentified single-engine configuration, resulting in an irreversible loss of speed.