As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING SKIN FLANGE FOR PANEL 522CT CORRODED. BLENDED IAW SRM 57-14-12 FIG 401U/T E/C IAW NTM NO CRACKS FOUND. INSTALLED SRM 51-25-01 FABRICATION COVER ON W/C 2000-206 MATERIAL THICKNESS: 0.753 MATERIAL REMOVED: 0.009 WITHIN LIMITS AS PER SRM: 57-14-12 FIG 301.