No fatalities

Left Main Landing Gear Strut Collapses During Landing After Unsafe Indication (N6543V)

Camarillo, CA, US

On October 12, 2003, a Cessna 172RG (registration N6543V) was involved in an aviation accident near Camarillo, CA. No fatalities were reported. Investigators recorded the probable cause as: The fracture and failure of the left landing gear actuator. Contributing to the accident was the operator's failure to comply with the manufacturer's service bulletin. 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

An airplane's left main landing gear strut collapsed on landing, causing a runway excursion. The pilot had heard a clank and received an unsafe gear indication, then returned to the departure airport for a landing attempt. Post-accident examination revealed fractured actuator components consistent with overload, and a relevant service bulletin was not complied with.

Incident Overview

During landing, the left main landing gear strut collapsed, causing the airplane to depart the runway to the left. The pilot had previously heard a "clank" sound while airborne, which he considered unusual. When the landing gear was lowered, an unsafe indication for the left main strut appeared. The pilot decided to return to the airport from which he had departed. After troubleshooting and circling the airport, the pilot made a landing attempt with the gear down.

Post-Accident Examination

Examination of the landing gear strut actuator body revealed numerous fractures and signs consistent with an overload event. The manufacturer had issued a Service Bulletin (SB) directing rework and inspection of the landing gear actuator for cracks at the location of the failures found on the accident actuator. The SB required compliance at 3,000 hours total time and at each 500-hour interval thereafter. The SB advised that failure to comply could result in failure of the actuator.

Maintenance Records

Review of the airplane's maintenance logbooks did not show compliance with the subject Service Bulletin. The airframe had accumulated a total time in service of 7,171 hours.

Frequently asked questions

What happened in the 12 Oct 2003 Cessna 172RG accident near Camarillo, CA?

An airplane's left main landing gear strut collapsed on landing, causing a runway excursion. The pilot had heard a clank and received an unsafe gear indication, then returned to the departure airport for a landing attempt. Post-accident examination revealed fractured actuator components consistent with overload, and…

Were there any fatalities in the 12 Oct 2003 Cessna 172RG accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 12 Oct 2003 involved a Cessna 172RG, registration N6543V, at Camarillo, CA.

What was the probable cause of the accident?

The fracture and failure of the left landing gear actuator. Contributing to the accident was the operator's failure to comply with the manufacturer's service bulletin.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20031015X01735. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.