Casualties unknown

Engine Failure and Gear-Up Landing Following Connecting Rod Fatigue (N2541Q)

Smithville, TX, US

On October 2, 1983, a Piper PA-28R-201T (registration N2541Q) was involved in an aviation accident near Smithville, TX. Investigators recorded the probable cause as: The #4 connecting rod failed due to fatigue, with a single fatigue initiation site at a change in contour on the flange end, along with oxide inclusions and forging defects. 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 2026-07-04Data APIEditorial standards

During cruise at 8,500 ft, an aircraft's engine failed. An emergency landing was made at an airport just overflown. Due to oil on the windshield, the pilot delayed gear extension, resulting in insufficient time for the right main and nose gear to lock. Touchdown occurred 366 ft beyond the threshold.

Engine Failure and Emergency Landing

During cruise at an altitude of 8,500 feet MSL, the aircraft's engine stopped operating. The pilot executed a night emergency landing at an airport that the aircraft had just flown over. On final approach, the pilot experienced difficulty seeing through the windshield due to an accumulation of oil on its surface.

Landing Gear Extension

The pilot delayed lowering the landing gear until a landing on the runway was assured. After crossing a road located in front of the runway, the pilot initiated gear extension. However, there was insufficient time for the right main landing gear and the nose gear to lock into the down position before touchdown.

Touchdown

The aircraft touched down 366 feet beyond the runway threshold.

Engine Examination

An engine teardown and metallurgical examination revealed that the #4 connecting rod had failed due to fatigue. Scanning electron microscope (SEM) examination of the origin area showed a single fatigue initiation site at a change in contour on the flange end. This irregular contour was not present on the other three flange ends. Additionally, oxide inclusions and forging defects were found along the original rod surface.

Probable cause

The #4 connecting rod failed due to fatigue, with a single fatigue initiation site at a change in contour on the flange end, along with oxide inclusions and forging defects.

Frequently asked questions

What happened in the 2 Oct 1983 Piper PA-28R-201T accident near Smithville, TX?

During cruise at 8,500 ft, an aircraft's engine failed. An emergency landing was made at an airport just overflown. Due to oil on the windshield, the pilot delayed gear extension, resulting in insufficient time for the right main and nose gear to lock. Touchdown occurred 366 ft beyond the threshold.

What aircraft was involved and where did it happen?

The accident on 2 Oct 1983 involved a Piper PA-28R-201T, registration N2541Q, at Smithville, TX.

What was the probable cause of the accident?

The #4 connecting rod failed due to fatigue, with a single fatigue initiation site at a change in contour on the flange end, along with oxide inclusions and forging defects.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X44832. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.