Aircraft runway excursion following nose gear actuator failure

Casualties unknown • Palestine, TX, US

A pilot experienced a violent jerking motion during the landing roll of a nose wheel touchdown, resulting in the aircraft departing the runway.

What happened

During the landing roll, as the nose wheel made contact with the runway, the pilot experienced a hard bump followed by a violent jerking motion to the left. This sequence caused the aircraft to depart the runway before coming to a stop.

The investigation

Upon removal of the engine cowling and examination of the engine mount, investigators discovered that the right side of the nose gear actuator aft attach point had separated from the tube cluster on the mount assembly. The actuator was found pushed aft into the firewall. Additionally, a section of the firewall located aft of the nose landing gear actuator had been crushed upward and aft into the forward baggage compartment.

Examination of the separated surface of the nose gear actuator aft attach point using photographs and stereoscopic magnification revealed signatures consistent with overload.

Findings

Investigation determined that Service Bulletin No. 1103, issued by the manufacturer for the inspection or replacement of the engine mount, had not been performed on this aircraft. The owner/pilot reported that the service bulletin was scheduled to be completed during the next maintenance visit.

Probable cause

The separation of the nose gear actuator aft attach point from the engine mount due to structural overload.

Frequently asked questions

What happened in the 2002-05-18 Piper PA-46-350P accident near Palestine, TX?

A pilot experienced a violent jerking motion during the landing roll of a nose wheel touchdown, resulting in the aircraft departing the runway.

What aircraft was involved and where did it happen?

The accident on 2002-05-18 involved a Piper PA-46-350P, registration N529TX, at Palestine, TX.

What was the probable cause of the accident?

The separation of the nose gear actuator aft attach point from the engine mount due to structural overload.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020530X00774. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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