Casualties unknown

1982-05-25: Cessna 310R (N3232M) — Excel Foundry — Evansville, IN

Evansville, IN, US

On May 25, 1982, a Cessna 310R (registration N3232M) operated by Excel Foundry was involved in an aviation accident near Evansville, IN. Investigators recorded the probable cause as: The collapse of the right landing gear was caused by the failure of the landing gear rod assembly (PN 0840125-15) due to overload, with no evidence of fatigue present. 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

The right landing gear collapsed shortly after touchdown during an instrument landing system approach. A metallurgical examination of the failed rod assembly revealed indications of overload, with no evidence of fatigue found.

What happened

The aircraft was conducting an instrument landing system (ILS) approach and successfully touched down on the runway. Shortly after landing, tower personnel contacted the pilot via radio to ask if he could make the first available taxiway turnoff. Immediately following this exchange, the right main landing gear collapsed.

The investigation

investigators conducted a detailed examination of the failed components. The failure originated in the landing gear rod assembly, specifically part number 0840125-15. A metallurgical analysis was performed on the fractured surface of the rod to determine the nature of the failure.

Findings

The metallurgical examination provided clear evidence regarding the cause of the structural failure. The results indicated that the rod assembly failed due to overload. Crucially, the analysis found no evidence of fatigue in the material, ruling out progressive crack growth or material degradation as primary factors. The failure appears to have been a sudden event rather than the result of long-term wear.

Safety message

This incident highlights the importance of structural integrity in landing gear components. While overload can occur due to excessive forces during landing operations, the absence of fatigue suggests that routine inspection protocols must also account for potential single-event overloads or manufacturing defects that might not show typical fatigue patterns.

Probable cause

The collapse of the right landing gear was caused by the failure of the landing gear rod assembly (PN 0840125-15) due to overload, with no evidence of fatigue present.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020917X02936. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.