Casualties unknown

1983-05-06: Cessna 421C (N3237U) — Gainesville, FL

Gainesville, FL, US

On May 6, 1983, a Cessna 421C (registration N3237U) was involved in an aviation accident near Gainesville, FL. Investigators recorded the probable cause as: Failure of the rod end connecting the nose gear to the actuator due to fatigue cracking originating from a corroded thread runout with a radius below specification. 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 1781061362Data APIEditorial standards

During landing, the nose gear collapsed when the aircraft settled on its nose. Investigation found the connecting rod end failed due to fatigue cracking from a corroded thread runout with a radius below specification.

Event Description

During takeoff, the aircrew heard an unusual 'thud' sound as the landing gear was retracting, but all gear indications were normal. Prior to landing at the destination, three green lights were observed when the landing gear switch was moved to the extend position. A normal touchdown was made, but when the nose was lowered, the aircraft settled on its nose.

Investigation Findings

An investigation revealed that the rod end, part number MS21242S4K, which connects the nose gear to the nose gear actuator, had failed. A metallurgical examination showed signs of high stress fatigue cracking over half of the fracture surface. The fatigue originated in the curve of a thread runout that was corroded. The radius of the curved surface measured 0.056 inch, while the specification MS-21242 required a minimum radius of 0.063 inch.

System Operation

Since the down position switch was connected to the actuator, it had indicated a safe indication when the actuator had operated to the extended position. However, with the rod end failure, the nose gear was hanging in a locked position.

Probable cause

Failure of the rod end connecting the nose gear to the actuator due to fatigue cracking originating from a corroded thread runout with a radius below specification.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001214X43083. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.