2 fatalities

Nighttime Engine Failure and Crash After Takeoff from Bogotá-El Dorado (N714CK)

Bogotá-El Dorado, ColombiaTakeoff (climb)

On July 7, 2008, a Boeing 747-200 (registration N714CK) operated by Kalitta Air was involved in an aviation accident near Bogotá-El Dorado, Colombia during takeoff. 2 people were killed. Investigators recorded the probable cause as: The inability of the accident aircraft to maintain flight after the loss of power of two engines. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 9 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
Aircraft registered N714CK
Aircraft registered N714CK. Photo: Iamthestig / CC BY 3.0, via Wikimedia Commons

An aircraft crashed into a farm after losing power on two engines shortly after a nighttime takeoff from Bogotá-El Dorado. All eight crew members were injured, and two people on the ground were killed.

Incident Overview and Immediate Aftermath Shortly after departing Bogotá-El Dorado Airport at night, the crew reported engine problems to air traffic control and was cleared to return immediately. The aircraft was unable to complete the return and attempted an emergency landing. It collided with a farm and crashed in an open field, where it was totally destroyed by impact forces. ## Casualties All eight crew members were injured, with five sustaining serious injuries. Two people in the farm were killed. ## Official Findings The official investigation identified the probable cause as the aircraft's inability to maintain flight after losing power on two engines. A non-recoverable surge on engine number 4 during rotation caused the loss of power on that engine. Contributing factors included an inefficient high-pressure turbine, excessive blade-tip clearance, reduced chord of the fan blades and leading edges, and the effects of high altitude. An undetermined anomaly in engine number 1, which appeared during extra power use, caused the loss of power on that engine. Inadequate operation of engine number 1 to maintain proper speed during ascent led to extra power use, which exposed the anomaly.