No fatalities

Landing Gear Fracture Due to Manufacturing Defect (N237SM)

Tampa, FL, US

On April 25, 2002, a Cessna 421C (registration N237SM) was involved in an aviation accident near Tampa, FL. No fatalities were reported. Investigators recorded the probable cause as: Fatigue cracking of the upper barrel (p/n 5141002-11) above a brazed-on collar, resulting from improper machining after assembly during the manufacturing process. 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 2026-09-04Data APIEditorial standards

A pilot aborted a landing after detecting a mechanical issue with the left main gear. After burning off fuel, he landed on grass using the nose and right gears. Investigation revealed fatigue cracking in the upper barrel caused by improper machining during assembly.

Incident Overview

Following a landing attempt, the pilot reported an abnormal touchdown and immediately recognized a mechanical problem. The pilot aborted the approach and cycled the landing gear twice. During this process, the gear unsafe light remained illuminated, indicating a persistent issue with the system.

Operational Response

The aircraft returned to the departure airport for further assessment. Tower personnel visually confirmed damage to the left main landing gear. To reduce weight and risk, the pilot proceeded to burn off approximately one and a half hours of fuel before attempting another landing. The final touchdown occurred on the grass adjacent to the paved runway, utilizing only the nose gear and the right main landing gear.

Technical Findings

Subsequent examination of the landing gear components identified the root cause of the failure. The upper barrel, designated by part number 5141002-11, fractured due to fatigue cracking. This cracking occurred above a brazed-on collar. The investigation determined that the fracture resulted from improper machining performed after the barrel was assembled during the manufacturing process.

Probable cause

Fatigue cracking of the upper barrel (p/n 5141002-11) above a brazed-on collar, resulting from improper machining after assembly during the manufacturing process.

Frequently asked questions

What happened in the 25 Apr 2002 Cessna 421C accident near Tampa, FL?

A pilot aborted a landing after detecting a mechanical issue with the left main gear. After burning off fuel, he landed on grass using the nose and right gears. Investigation revealed fatigue cracking in the upper barrel caused by improper machining during assembly.

Were there any fatalities in the 25 Apr 2002 Cessna 421C accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 25 Apr 2002 involved a Cessna 421C, registration N237SM, at Tampa, FL.

What was the probable cause of the accident?

Fatigue cracking of the upper barrel (p/n 5141002-11) above a brazed-on collar, resulting from improper machining after assembly during the manufacturing process.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020429X00586. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.