Aviation Accident Summaries

Aviation Accident Summary MIA89FA093

INVERNESS, FL, USA

Aircraft #1

N43330

PIPER PA-28R-200

Analysis

DURING CRUISE FLT A TOTAL LOSS OF ENGINE POWER WAS EXPERIENCED. THE PLT WAS ATTEMPTING A FORCED LANDING WHEN THE ACFT CONTACTED ELECTRICAL WIRES AND A TREE PRIOR TO COLLIDING WITH THE TERRAIN. POST ACCIDENT INSPECTION REVEALED THE PROPELLER GOVERNOR OIL LINE CRACKED TO THE POINT THAT ENGINE OIL PUMPED OUT OF THE ENGINE WHICH SUBSEQUENTLY SEIZED. THE OIL LINE WAS INSTALLED AFTER ENGINE OVERHAUL WITHOUT TWO CLAMPS AND WAS BENT IN THE AREA WHERE THE ALTERNATOR BELT IS ADJUSTED. THE BENDING DAMAGE CAUSED A FATIGUE CRACK IN THE LINE AND THE LACK OF SUPPORT CLAMPS AIDED IN THE CRACKING PROCESS.

Probable Cause and Findings

THE FAILURE OF THE PROPELLER GOVERNOR OIL LINE DUE TO FATIGUE WHICH WAS CAUSED BY BENDING DAMAGE TO THE LINE AND THE FAILURE OF MECHANICS TO INSTALL SUPPORT CLAMPS ON THE LINE WHICH CAUSED THE FATIGUE TO PROPAGATE AT A FASTER RATE.

 

Source: NTSB Aviation Accident Database

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