As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C2 CHECK - CORROSION ON LOWER STUB WALL MOUNT PLATE. REMOVED CORROSION FROM THE MOUNT PLATE IAW SRM 51-21-00. 4 FASTENERS REMOVED IAW SRM 51-42-45. MATERIAL LOSS .003", MAX ALLOWED .005" FOUND TO BE WITHIN LIMITS IAW ENGINEERING DRG 224844 SHT A, REV A AND SRM 51-14-00 REPAIR 3. INSTALLED FASTENERS IAW SRM 51-42-45. APPLIED ALONDINE AND PRIMER IAW SRM 51-21-10 AND 51-25-10.