2 fatalities

2008-07-07: Boeing 747-200 (N714CK) — Kalitta Air — Bogotá-El Dorado, Colombia

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 aircraft lost sufficient power to maintain flight due to a surge in engine number 4 and an unidentified anomaly in engine number 1 during the climb. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 13 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781197342Data APIEditorial standards
Aircraft registered N714CK
Aircraft registered N714CK. Photo: Iamthestig / CC BY 3.0, via Wikimedia Commons

An aircraft crashed in an open field near Bogotá after experiencing significant engine issues during its initial climb, resulting in fatalities on the ground.

What happened

During a nighttime departure from Bogotá-El Dorado Airport, the flight crew encountered critical mechanical difficulties while climbing. The crew notified Air Traffic Control of engine malfunctions and received clearance to perform an immediate return to the airport. However, as the aircraft was unable to maintain its altitude, the pilot attempted an emergency landing. During this maneuver, the aircraft struck a farm before crashing in an open field. The impact resulted in the total destruction of the aircraft. While all 8 crew members survived the crash with injuries—including five who were seriously hurt—the collision caused the deaths of two people located on the farm.

Findings

Investigations determined that the accident occurred because the aircraft could not sustain flight following the loss of power in two engines. The primary cause was a non-recoverable surge in engine number 4 during the rotation phase, which led to a loss of thrust. This surge was driven by several factors, including high-altitude effects, excessive blade-tip clearance, and an inefficient high-pressure turbine, alongside reduced chord on the fan blades and leading edges. Additionally, an unidentified anomaly occurred in engine number 1 when extra power was required during the ascent. The need for increased power to compensate for the climb exposed this malfunction, which ultimately led to the loss of power in that engine as well.

Probable cause

The aircraft lost sufficient power to maintain flight due to a surge in engine number 4 and an unidentified anomaly in engine number 1 during the climb.