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 Nº: ZL-500-03-1-001 EWIS AT LH WING TOP SKIN PANEL 2, LOWER SURFACE TRAILING EDGE OVERHANG AT RIBS 14-15 CORROSION WAS FOUND. DUE THE CORROSION IS OUT SRM ADL DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AIRBUS PROVIDED REPAIR INSTRUCTION UNDER DOSSIER81191642. COOPESA PERFORMED REPAIR UNDER EO COO-EO-2023-17438-R00.