Service difficulty report · Engine

Difficulty date
June 2, 2005
Submitted
June 23, 2005
Operation
General aviation
Engine
Cont IO520D
Part
Engine
Condition
Making Metal
Stage of operation
TX
How discovered
O
Nature of condition
J
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

FACTORY REBUILT ENGINE WAS INSTALLED ON THE AIRFRAME. DURING THE GROUND RUNS, LEAK CHECKS AND FINAL ADJUSTMENTS, THE MECHANIC NOTED THE PROP GOVERNOR WAS NOT CONTROLLING THE PROP AS IT SHOULD. AFTER PERFORMING CHECKS RECOMMENDED BY THE MFG, PROP WAS REMOVED AND METAL FLAKES WERE NOTED IN THE END OF THE CRANKSHAFT. THE OIL FILTER WAS REMOVED AND INSPECTED AND WHAT APPEARED TO BE BRONZE, AND STEEL PARTICLES WERE FOUND. THE FILTER ALONG WITH AN OIL SAMPLE WERE SUBMITTED TO THE ENGINE MFG. REQUESTED THE ENGINE BE RETURNED TO THEM FOR FURTHER ANALYSIS.