Casualties unknown

Left Main Gear Axle Failure During Touch-and-Go Landing (N8239A)

Frederick, MD, US

On August 16, 1990, a Cessna 170B (registration N8239A) operated by Jon R. Shomer, JR was involved in an aviation accident near Frederick, MD. Investigators recorded the probable cause as: The left main gear axle fractured due to fatigue corrosion at the flange junction, which caused the aircraft to ground loop during the landing roll. 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 2026-06-22Data APIEditorial standards

The left main gear axle fractured during the landing roll of an eleventh touch-and-go, causing the aircraft to ground loop due to fatigue corrosion.

What happened

The pilot was conducting his eleventh touch-and-go landing when the left main gear axle failed during the landing roll. This mechanical failure caused the aircraft to ground loop.

The investigation

Examination of the aircraft revealed that the axle was fractured at its flange junction. A metallurgical examination confirmed the presence of fatigue corrosion on the fracture surface.

Findings

The structural integrity of the left main gear axle was compromised by fatigue corrosion, leading to a sudden failure under landing loads.

Probable cause

The left main gear axle fractured due to fatigue corrosion at the flange junction, which caused the aircraft to ground loop during the landing roll.

Frequently asked questions

What happened in the 16 Aug 1990 Cessna 170B accident near Frederick, MD?

The left main gear axle fractured during the landing roll of an eleventh touch-and-go, causing the aircraft to ground loop due to fatigue corrosion.

What aircraft was involved and where did it happen?

The accident on 16 Aug 1990 involved a Cessna 170B, registration N8239A, operated by Jon R. Shomer, JR, at Frederick, MD.

What was the probable cause of the accident?

The left main gear axle fractured due to fatigue corrosion at the flange junction, which caused the aircraft to ground loop during the landing roll.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X23905. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.