As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HEAVY MAINTENANCE CHECK, CORROSION WAS REPORTED ON THE TOP SKIN PANEL 2 RIB-6-9, OF THE T/E OVERHANG. REMOVED CORROSION IAW SRM 51-74-00. JACKED ACFT AND REMOVED CORROSION FROM RT WING TOP SKIN AT THE T/E LOWER SURFACE RIB 7A. ACCOMPLISHED FINAL REPAIR IAW AIRBUS TD-J1-S2-31246-2014 ISSUE "B" AND EA PT20-57-029 WITH A14-654-01.