Engine failure and crash near Belize City-Philip S. W. Goldson Airport

1 fatality • Belize City-Philip S. W. Goldson, Belize • Takeoff (climb)

An aircraft experienced a left engine failure during its initial climb from Belize City, resulting in a stall and subsequent crash into a wooded area.

What happened

During the takeoff phase from Belize City-Philip S. W. Goldson Airport, the aircraft experienced a mechanical failure involving the left engine. As the plane attempted to climb, the loss of power caused the aircraft to bank heavily to the left. This maneuver led to an aerodynamic stall, causing the plane to descend into a densely forested region situated close to the airport perimeter.

The impact resulted in the total destruction of the aircraft. Among the occupants, one fatality was recorded involving a crew member, while the second pilot sustained injuries during the event.

Findings

Investigations into the crash revealed that the aircraft was operating at a weight exceeding its maximum takeoff weight by 500 pounds. This overloading of the aircraft was identified as a significant factor that likely contributed to the failure of the left engine during the critical climb period.

Probable cause

The engine failure occurred shortly after rotation while the aircraft was operating above its maximum allowable takeoff weight.

Frequently asked questions

What happened in the 1962-01-06 Curtiss C-46 Commando accident near Belize City-Philip S. W. Goldson, Belize?

An aircraft experienced a left engine failure during its initial climb from Belize City, resulting in a stall and subsequent crash into a wooded area.

Were there any fatalities in the 1962-01-06 Curtiss C-46 Commando accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 1962-01-06 involved a Curtiss C-46 Commando, registration HR-TNB, operated by TAN Airlines - Transportes Aéreos Nacionales de Honduras, at Belize City-Philip S. W. Goldson, Belize.

What was the probable cause of the accident?

The engine failure occurred shortly after rotation while the aircraft was operating above its maximum allowable takeoff weight.

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