No fatalities

Piper PA-32R Engine Failure and Emergency Landing at Lille-Lesquin (F-GGBD)

FR

On September 15, 2013, a PIPER PA-32R (registration F-GGBD) was involved in an aviation accident near FR. No fatalities were reported. Investigators recorded the probable cause as: The rupture of the connecting rod was likely due to a lubrication defect, probably caused by an improperly locked oil filler cap leading to a leak. This summary draws on records from the French Bureau d'Enquêtes et d'Analyses (BEA).

Sourcesthe French Bureau d'Enquêtes et d'Analyses (BEA)Primary reportUpdated 2026-10-18Data APIEditorial standards

In September 2013, a Piper PA-32R (F-GGBD) experienced severe engine vibrations and oil leakage during a local flight. The pilot declared an emergency and landed safely at Lille-Lesquin. Investigation linked the failure to inadequate lubrication.

Incident Overview

On September 15, 2013, around 14:30 local time, a private Piper PA-32R with registration F-GGBD was involved in an incident at Lille-Lesquin airport. The aircraft was operated by its owner-pilot for personal convenience. During the event, the engine sustained damage, but no injuries were reported to the pilot on board.

Flight Progression

The pilot had completed a thirty-minute local flight and initiated two traffic pattern circuits on runway 20. While in the early downwind phase of the second circuit, the pilot observed significant vibrations originating from the engine. This was immediately followed by oil spraying onto the cowling and the presence of smoke. Recognizing the severity of the situation, the pilot declared an emergency and executed a landing on runway 08.

Technical Findings

Post-incident inspection revealed a perforation in the upper crankcase near cylinder number 6. The investigation determined that the engine damage resulted from the failure of connecting rod number 6, which was fractured in multiple locations. The manufacturer attributed this mechanical failure to a lubrication defect. Additionally, an oil puddle was found at the pre-flight start-up location, and the oil filler cap was observed to be present but not locked.

Conclusion

The investigation concluded that the connecting rod rupture was likely caused by insufficient lubrication. It is probable that an improperly secured oil filler cap led to a leak, which subsequently resulted in the lubrication failure.

Probable cause

The rupture of the connecting rod was likely due to a lubrication defect, probably caused by an improperly locked oil filler cap leading to a leak.

Frequently asked questions

What happened in the 15 Sept 2013 PIPER PA-32R accident near FR?

In September 2013, a Piper PA-32R (F-GGBD) experienced severe engine vibrations and oil leakage during a local flight. The pilot declared an emergency and landed safely at Lille-Lesquin. Investigation linked the failure to inadequate lubrication.

Were there any fatalities in the 15 Sept 2013 PIPER PA-32R accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 15 Sept 2013 involved a PIPER PA-32R, registration F-GGBD, at FR.

What was the probable cause of the accident?

The rupture of the connecting rod was likely due to a lubrication defect, probably caused by an improperly locked oil filler cap leading to a leak.