As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AROUND SCREW HOLES OF MATING SURFACE ON PANEL 522BT. REMOVED CORROSION AND ALODINED MIN THICKNESS REMAINING .217, PANEL IS WITHIN LIMITS IAW SRM 57-10-35-02-02, REV 12. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1, REV 7. APPLIED ALODINE AND PRIMED REWORKED AREAS IAW SRM REV 12 57-10-35-02-02. COMPLIED WITH STEP 7 OF SRM 57-10-35-02-02, REV 12.