Casualties unknown

Engine Failure and Crash Landing Due to Fuel Pump Housing Failure (N4732S)

Igiugig, AK, US

On June 2, 1984, a Piper PA-32-260 (registration N4732S) was involved in an aviation accident near Igiugig, AK. Investigators recorded the probable cause as: The failure of the engine-driven fuel pump housing, which resulted in the loss of engine power during flight. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-06-20Data APIEditorial standards

A pilot experienced an in-flight engine failure after hearing a loud bang, resulting in a crash landing on tundra that damaged the nose gear, left main gear, wing, and propeller. Investigation confirmed the engine-driven fuel pump housing had failed.

What happened

During flight operations, the pilot reported hearing a loud bang followed by an immediate loss of engine power. In response to the emergency, the pilot transmitted a mayday call and initiated an emergency landing procedure on rolling tundra terrain. The impact forces caused significant structural damage during the landing sequence. Specifically, both the nose gear and the left main landing gear collapsed upon touchdown. Additionally, the aircraft's wing and propeller sustained damage from the crash.

The investigation

A post-accident examination of the airframe and propulsion system was conducted to determine the root cause of the mechanical failure. Inspectors focused on the fuel delivery system components. The inspection revealed that the housing for the engine-driven fuel pump had failed structurally. This failure compromised the fuel supply necessary for continued engine operation.

Findings

The investigation identified several key factors contributing to the accident sequence. The primary mechanical issue was the failure of the engine-driven fuel pump housing. This component failure directly led to the sudden loss of power during flight. Furthermore, the pilot did not recall operating the electric fuel pump at the time the engine lost power. The lack of backup fuel pressure likely prevented any potential recovery or continued flight after the initial mechanical failure.

Safety message

Pilots should be aware that failures in critical fuel system components can occur without warning. It is essential to verify the operation of backup systems, such as electric fuel pumps, immediately upon experiencing engine anomalies. Proper emergency procedures and awareness of backup fuel sources are vital for managing in-flight power loss scenarios.

Probable cause

The failure of the engine-driven fuel pump housing, which resulted in the loss of engine power during flight.

Frequently asked questions

What happened in the 2 Jun 1984 Piper PA-32-260 accident near Igiugig, AK?

A pilot experienced an in-flight engine failure after hearing a loud bang, resulting in a crash landing on tundra that damaged the nose gear, left main gear, wing, and propeller. Investigation confirmed the engine-driven fuel pump housing had failed.

What aircraft was involved and where did it happen?

The accident on 2 Jun 1984 involved a Piper PA-32-260, registration N4732S, at Igiugig, AK.

What was the probable cause of the accident?

The failure of the engine-driven fuel pump housing, which resulted in the loss of engine power during flight.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X39791. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.