No fatalities

2002-02-11: Lockheed C-130 Hercules (148895) — United States Marine Corps (USMC) — Twentynine Palms, United States of America

Twentynine Palms, United States of AmericaTakeoff (climb)

On February 11, 2002, a Lockheed C-130 Hercules (registration 148895) operated by United States Marine Corps (USMC) was involved in an aviation accident near Twentynine Palms, United States of America during takeoff. No fatalities were reported. Investigators recorded the probable cause as: The combination of an initial engine failure and a secondary loss of power on another engine while at maximum takeoff weight made it impossible to maintain altitude. 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 1781202075Data APIEditorial standards

A training flight departing from Twentynine Palms resulted in an emergency landing after multiple engine failures prevented the aircraft from maintaining altitude.

What happened

During a local training mission originating from Twentynine Palms, the aircraft experienced a series of mechanical issues shortly after departure. The sequence began when the number one engine failed during the initial climb phase. Following this primary failure, the number four engine also lost power, making it difficult for the crew to sustain sufficient altitude.

Due to the loss of propulsion, the crew performed an emergency landing in a sandy terrain situated approximately 4.5 km beyond the runway threshold. While the aircraft sustained damage that rendered it a total loss, there were no injuries reported among the eight crew members on board.

Findings

Investigations into the incident identified that the aircraft was operating at its maximum takeoff weight during the flight. The primary contributing factors included the failure of engine number one and the subsequent loss of power in engine number four, which prevented the plane from maintaining a positive rate of climb.

Probable cause

The combination of an initial engine failure and a secondary loss of power on another engine while at maximum takeoff weight made it impossible to maintain altitude.