Event Description
During the flight, the pilot observed a gradual decrease in engine power. The application of carburetor heat did not restore power. Subsequently, a loud noise was heard, prompting the pilot to shut down the engine. During the ensuing forced landing, the nose gear collapsed and the aircraft nosed over.
Examination Findings
An examination of the engine revealed that the No. 4 connecting rod had failed. Internal damage was attributed to a lack of lubrication. Further inspection determined that the diaphragm of an oil pressure switch had ruptured, allowing the engine oil supply to deplete. The switch, Datcon part number 40558-1, had been installed directly into the engine block's tapped oil gallery hole on January 1, 1974, and was used in connection with the electrical operation of the aircraft's hourmeter. Additionally, it was found that Datcon Service Bulletin #1, titled "Hazardous Installation of Oil Pressure Switches" and dated January 2, 1975, had not been complied with.