1 fatality

1962-01-06: Curtiss C-46 Commando (HR-TNB) — TAN Airlines - Transportes Aéreos Nacionales de Honduras — Belize City-Philip S. W. Goldson, Belize

Belize City-Philip S. W. Goldson, BelizeTakeoff (climb)

On January 6, 1962, a Curtiss C-46 Commando (registration HR-TNB) operated by TAN Airlines - Transportes Aéreos Nacionales de Honduras was involved in an aviation accident near Belize City-Philip S. W. Goldson, Belize during takeoff. One person was killed. Investigators recorded the probable cause as: Failure of the left engine shortly after rotation and aircraft overloaded. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781245150Data APIEditorial standards

Shortly after takeoff from Belize City Airport, the left engine failed, causing the aircraft to bank left, stall, and crash in a wooded area. One crew member died, one pilot was injured. The aircraft was overloaded by 500 pounds.

Accident Overview

The accident sequence began immediately after the aircraft took off from Belize City-Philip S. W. Goldson Airport. During the initial climb, the left engine ceased to operate. In response to the loss of thrust on one side, the airplane banked sharply to the left. The aircraft then lost airspeed and entered an aerodynamic stall. With insufficient altitude to recover, the airplane crashed into a densely forested area in the proximity of the airport.

The crash resulted in the destruction of the aircraft. One crew member suffered fatal injuries, while the other pilot sustained non-fatal injuries.

An investigation into the accident was conducted. It was established that at the time of departure, the aircraft's gross weight exceeded the maximum takeoff weight by 500 pounds. This overweight condition was considered likely to have contributed to the failure of the left engine.

Probable Cause

The official probable cause was determined to be failure of the left engine shortly after rotation and aircraft overloaded.