Casualties unknown

Engine Failure During Fuel Tank Switch Leads to Emergency Landing in River Bed (N8956N)

Gustavus, AK, US

On June 15, 1996, a Piper PA-32-300 (registration N8956N) was involved in an aviation accident near Gustavus, AK. Investigators recorded the probable cause as: A loss of engine power due to low fuel pressure from the engine driven fuel pump and subsequent fuel starvation. A factor was the lack of suitable terrain for a forced landing. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A pilot experienced engine failure after switching fuel tanks and turning on the electric fuel pump during cruise. Examination revealed a faulty engine-driven fuel pump that did not meet pressure specifications.

Incident Overview

During cruise flight at 5,000 feet, the pilot was operating with the fuel selector positioned on the left main fuel tank, which contained approximately 12 gallons of fuel. The pilot's intention was to deplete the fuel in the left main tank before switching to another tank. After noting a slight loss of fuel pressure, the pilot proceeded to switch the fuel selector to the right main tank, which contained about 10 gallons. Concurrently, the pilot turned the electric fuel pump to the 'on' position.

Engine Failure

Following the tank switch and activation of the electric fuel pump, the fuel pressure dropped to zero and the engine ceased operation. The pilot then selected the right auxiliary fuel tank but was unable to restart the engine.

Emergency Landing and Damage

The pilot conducted an emergency landing in a river bed. During the landing, the right wing struck a small bank, resulting in damage to the nose gear, propeller, right main landing gear, and the right wing.

Post-Accident Examination

An examination of the engine revealed that upon activation of the electric fuel pump, it produced fuel to the engine-driven pump. However, hand rotation of the engine did not produce any fuel flow from the engine-driven fuel pump. Further examination of the engine-driven fuel pump on a test bench indicated that it did not meet the minimum fuel pressure as prescribed by the manufacturer and was very hard to prime.

All Piper PA-32 accidents →

Frequently asked questions

What happened in the 15 Jun 1996 Piper PA-32-300 accident near Gustavus, AK?

A pilot experienced engine failure after switching fuel tanks and turning on the electric fuel pump during cruise. Examination revealed a faulty engine-driven fuel pump that did not meet pressure specifications.

What aircraft was involved and where did it happen?

The accident on 15 Jun 1996 involved a Piper PA-32-300, registration N8956N, at Gustavus, AK.

What was the probable cause of the accident?

A loss of engine power due to low fuel pressure from the engine driven fuel pump and subsequent fuel starvation. A factor was the lack of suitable terrain for a forced landing.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001208X05893. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.