As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-500-03-1-002, CORROSION AT RH WING TEOH BETWEEN RIB 7 AND RIB 8 WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81140719. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB: A1M146 (ITEM 6-6)