Engine Power Loss and Gear Separation During Descent

Casualties unknown • Haslet, TX, US

An aircraft experienced a sudden loss of engine power during descent, leading to an emergency landing in a field that resulted in landing gear separation.

What happened

Approximately 40 minutes into the flight, while the Cessna (type not specified) was 4 miles south of its destination airport, the aircraft was in a normal descent when the propeller suddenly increased to maximum RPM. Shortly after this increase, the pilot observed the oil pressure light illuminate and noted that the oil pressure gauge indicated zero.

Following the loss of engine power, the pilot performed an emergency landing in a field located approximately 2 miles south of the runway threshold. The aircraft touched down on soft ground, which caused the landing gear to separate from the airframe. There were no injuries reported.

The investigation

A post-accident examination of the engine revealed that no oil remained within the engine. Investigators found that the internal element of the oil filter had collapsed inward and the oil filter converter plate gasket had separated from the plate and broken in half. Additionally, the oil filter bypass valve was found to have been installed improperly.

Probable cause

Excessive oil pressure caused by an improperly installed oil filter bypass valve led to the collapse of the oil filter element and the failure of the oil filter converter plate gasket, resulting in total loss of engine oil and subsequent engine power loss.

Frequently asked questions

What happened in the 2001-02-17 Piper PA32-R-301T accident near Haslet, TX?

An aircraft experienced a sudden loss of engine power during descent, leading to an emergency landing in a field that resulted in landing gear separation.

What aircraft was involved and where did it happen?

The accident on 2001-02-17 involved a Piper PA32-R-301T, registration N8355L, operated by Hest Aviation, at Haslet, TX.

What was the probable cause of the accident?

Excessive oil pressure caused by an improperly installed oil filter bypass valve led to the collapse of the oil filter element and the failure of the oil filter converter plate gasket, resulting in total loss of engine oil and subsequent engine power loss.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010301X00528. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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