Engine failure leads to forced landing of Miles Messenger near Bourges

Casualties unknown • Bourges/FRA, CH

A Miles Messenger aircraft experienced a critical engine failure during a flight from Geneva to Le Mans, resulting in a forced landing in France.

What happened

On July 19, 1961, a Miles Messenger, registration HB-EEC, was conducting a private pleasure flight from Geneva, Switzerland, to Le Mans, France. The aircraft was carrying the pilot and two passengers at the time of the incident. While flying near Bourges, France, the aircraft suffered a sudden engine failure. The pilot was forced to perform an emergency landing in the vicinity of Bourges. The landing was completed successfully at approximately 10:45 local time, and the aircraft sustained no significant damage beyond the engine failure.

The investigation

The investigation, which incorporated findings from the French civil aviation inspectorate and supplementary research conducted in Switzerland, focused on the mechanical cause of the power loss. Investigators examined the engine, a Cirrus Major 3, to determine why the propulsion system failed during flight.

Findings

The investigation established that the engine failure was caused by the failure of a connecting rod in the second cylinder. Specifically, the rod broke due to metal fatigue, which subsequently caused the component to penetrate the engine crankcase.

Probable cause

The engine failure was caused by the fatigue-induced breakage of a connecting rod in the second cylinder, which punctured the engine crankcase.

Frequently asked questions

What happened in the 1961-07-19 MILES AIRCRAFT LIMITED M.38 accident near Bourges/FRA, CH?

A Miles Messenger aircraft experienced a critical engine failure during a flight from Geneva to Le Mans, resulting in a forced landing in France.

What aircraft was involved and where did it happen?

The accident on 1961-07-19 involved a MILES AIRCRAFT LIMITED M.38, registration HB-EEC, at Bourges/FRA, CH.

What was the probable cause of the accident?

The engine failure was caused by the fatigue-induced breakage of a connecting rod in the second cylinder, which punctured the engine crankcase.

Investigation report by the Swiss Transportation Safety Investigation Board (STSB / SUST). Original record: https://www.sust.admin.ch/inhalte/AV-berichte/53.pdf. This page is a structured re-presentation; facts and quotes are in the Swiss Transportation Safety Investigation Board (STSB), Switzerland.

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