Fatal crash of aircraft following dual engine failure

50 fatalities • Holdcroft, United States of America • Flight

An aircraft crashed into a wooded area after experiencing the simultaneous failure of two engines during flight through icing conditions.

What happened

During a flight at 8,000 feet, the aircraft encountered heavy fog and icing. During this period, both engine number three and engine number four ceased functioning. The crew attempted to perform an engine restart procedure, but these efforts failed to restore power.

Following the loss of power, the aircraft became uncontrollable. It descended into a forested region, where it impacted the terrain in a level attitude with no forward momentum. The impact resulted in the total destruction of the aircraft and caused the deaths of all 50 occupants.

Findings

Investigations concluded that the primary factor in the accident was the delayed activation of engine ice-protection systems. Because these systems were not armed in a timely manner while flying through icing conditions, the engines lost power. This loss of power also led to a deficiency in the electrical energy necessary to unfeather the propellers and successfully relight enough engines to sustain controlled flight.

Probable cause

The failure to arm engine ice-protection systems promptly during icing conditions caused a loss of engine power and insufficient electrical energy for propeller unfeathering and engine relighting.

Frequently asked questions

What happened in the 1960-01-18 Vickers Viscount accident near Holdcroft, United States of America?

An aircraft crashed into a wooded area after experiencing the simultaneous failure of two engines during flight through icing conditions.

Were there any fatalities in the 1960-01-18 Vickers Viscount accident?

The accident was fatal, resulting in 50 fatalities.

What aircraft was involved and where did it happen?

The accident on 1960-01-18 involved a Vickers Viscount, registration N7462, operated by Capital Airlines (USA), at Holdcroft, United States of America.

What was the probable cause of the accident?

The failure to arm engine ice-protection systems promptly during icing conditions caused a loss of engine power and insufficient electrical energy for propeller unfeathering and engine relighting.

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