What was found
UPON DISASSEMBLY OF THE ENGINE TO REPAIR FOR REPORTED METAL IN OIL FOUND A CRACK IN THE PT OUTER SHAFT ORIGINATING AT THE CURVIC COUPLING END OF THE SHAFT. THE CRACK EXTENDED APPROXIMATELY 270 DEGREES AROUND THE SHAFT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON DISASSEMBLY OF THE ENGINE TO REPAIR FOR REPORTED METAL IN OIL FOUND A CRACK IN THE PT OUTER SHAFT ORIGINATING AT THE CURVIC COUPLING END OF THE SHAFT. THE CRACK EXTENDED APPROXIMATELY 270 DEGREES AROUND THE SHAFT.