Fatal crash following engine failure during takeoff

24 fatalities • Guayaramerín, Bolivia • Takeoff (climb)

An aircraft crashed into a heavily forested area shortly after departing, resulting in 24 fatalities and four injuries.

What happened

During the initial climb phase of flight, the aircraft experienced a sudden loss of power due to an engine malfunction. This mechanical failure caused the plane to lose altitude rapidly while ascending from the runway. The descent continued until the aircraft impacted a dense wooded area.

As a result of the impact, there were 24 fatalities among the passengers and crew, including women and children. Additionally, four individuals sustained injuries during the accident.

Findings

Investigations into the crash determined that the primary factor was an engine failure occurring during the early stages of the climb.

Probable cause

The engine failed during the initial climb phase for reasons that remain undetermined.

Frequently asked questions

What happened in the 1989-12-21 Lockheed C-130 Hercules accident near Guayaramerín, Bolivia?

An aircraft crashed into a heavily forested area shortly after departing, resulting in 24 fatalities and four injuries.

Were there any fatalities in the 1989-12-21 Lockheed C-130 Hercules accident?

The accident was fatal, resulting in 24 fatalities.

What aircraft was involved and where did it happen?

The accident on 1989-12-21 involved a Lockheed C-130 Hercules, registration TAM-62, operated by TAM Bolivia - Transporte Aéreo Militar Boliviano, at Guayaramerín, Bolivia.

What was the probable cause of the accident?

The engine failed during the initial climb phase for reasons that remain undetermined.

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