Aircraft crash during approach to Salvador-Dois de Julho Airport

No fatalities • Salvador, Brazil • Landing (descent or approach)

An aircraft experienced an engine malfunction during its final approach to Salvador, resulting in a crash in an open field with no fatalities.

What happened

During the final approach phase toward Salvador-Dois de Julho Airport, the flight crew encountered a significant technical issue involving the left engine. Specifically, the oil temperature in the left engine began to rise unexpectedly. In an effort to manage this thermal increase, the crew was required to decrease power to that engine.

This reduction in power led to a loss of airspeed, causing the aircraft type to stall while still on final approach. The plane subsequently impacted an open field near the airport. Despite the impact and the resulting damage to the airframe, which was determined to be beyond repair, all 54 occupants were successfully rescued from the wreckage without any reported fatalities or injuries.

Findings

Official investigations into the accident identified a technical issue with the left engine as the primary factor that led to the loss of control and subsequent stall during the approach.

Probable cause

A malfunction involving rising oil temperature in the left engine necessitated a power reduction that induced an aerodynamic stall.

Frequently asked questions

What happened in the 1965-12-19 Curtiss C-46 Commando accident near Salvador, Brazil?

An aircraft experienced an engine malfunction during its final approach to Salvador, resulting in a crash in an open field with no fatalities.

Were there any fatalities in the 1965-12-19 Curtiss C-46 Commando accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1965-12-19 involved a Curtiss C-46 Commando, registration PP-LDQ, operated by VASP - Viação Aérea de São Paulo, at Salvador, Brazil.

What was the probable cause of the accident?

A malfunction involving rising oil temperature in the left engine necessitated a power reduction that induced an aerodynamic stall.

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