Aircraft crash during takeoff climb

2 fatalities • Palma de Mallorca-Son Sant Juan, Spain • Takeoff (climb)

An aircraft crashed on an airport apron following an engine failure during its initial climb phase.

What happened

During the early stages of flight, an aircraft experienced a critical mechanical failure shortly after departing the runway. While the aircraft was performing its initial climb, the left engine ceased functioning properly. This loss of power caused the aircraft to lose necessary altitude, preventing it from maintaining flight.

As the aircraft descended, it struck the ground on the airport apron in the vicinity of several hangars. The impact occurred during the takeoff phase of the flight. The accident resulted in two fatalities, as both the pilot and the co-pilot were killed in the crash.

Findings

  • The primary factor in the loss of altitude was the failure of the left engine during the climb.

Probable cause

The failure of the left engine during the initial climb phase led to a loss of altitude and subsequent impact on the apron.

Frequently asked questions

What happened in the 1993-03-02 Douglas C-47 Skytrain (DC-3) accident near Palma de Mallorca-Son Sant Juan, Spain?

An aircraft crashed on an airport apron following an engine failure during its initial climb phase.

Were there any fatalities in the 1993-03-02 Douglas C-47 Skytrain (DC-3) accident?

The accident was fatal, resulting in 2 fatalities.

What aircraft was involved and where did it happen?

The accident on 1993-03-02 involved a Douglas C-47 Skytrain (DC-3), registration EC-FAH, operated by Tadair, at Palma de Mallorca-Son Sant Juan, Spain.

What was the probable cause of the accident?

The failure of the left engine during the initial climb phase led to a loss of altitude and subsequent impact on the apron.

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