As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION PITS APPROXIMENTLY 30 TO 50 PERCENT OF WALL THICKNESS. THIS PART ONLY 10 PERCENT OF WALL THICKNESS ALLOWED BY MFG. THIS PART IS MAGNESUM. THE PITTING IS UNDER THE FLET 35, ABOVE THE LOWER BUSHING, THE FELT IS SATURATED WITH MOISTURE AND GREASE WHICH ALLOWS CORROSION TO ATTACH THE PART. (K)