Engine failure and fire leading to fatal crash

2 fatalities • Spokane-Intl (Geiger Field), United States of America • Takeoff (climb)

A flight experienced an engine failure and subsequent fire shortly after takeoff, resulting in a fatal collision with terrain.

What happened

During the initial climb phase following takeoff, the crew identified a malfunction involving the right engine. The copilot notified air traffic control that the aircraft needed to return to the airport because the right engine had been shut down. Almost immediately after this report, the tower controller observed flames originating from the aircraft.

As the aircraft attempted to manage the emergency, it struck level ground approximately 3,450 feet beyond the end of runway 21. At the moment of impact, the aircraft type was in a steep nose-down descent, angled between 75° and 80°. The accident resulted in two fatalities, as both pilots were killed in the crash.

Findings

Post-accident investigations revealed that the propeller on the right engine was in the feathered position. While the left engine showed evidence of producing power during the descent, the right engine was non-operational. Investigators identified a fatigue crack that caused the head of the number eight cylinder on the right engine to separate from its barrel. No other mechanical malfunctions or failures were identified as contributing to the accident.

Probable cause

A fatigue crack in the number eight cylinder of the right engine caused a separation of the cylinder head from the barrel, leading to engine failure and fire.

Frequently asked questions

What happened in the 1994-03-18 Douglas DC-3 accident near Spokane-Intl (Geiger Field), United States of America?

A flight experienced an engine failure and subsequent fire shortly after takeoff, resulting in a fatal collision with terrain.

Were there any fatalities in the 1994-03-18 Douglas DC-3 accident?

The accident was fatal, resulting in 2 fatalities.

What aircraft was involved and where did it happen?

The accident on 1994-03-18 involved a Douglas DC-3, registration N3433Y, operated by Salair, at Spokane-Intl (Geiger Field), United States of America.

What was the probable cause of the accident?

A fatigue crack in the number eight cylinder of the right engine caused a separation of the cylinder head from the barrel, leading to engine failure and fire.

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