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 TASK Nº: 534107-01-1-001_P1-OP-UP/0 CPCP, IT WAS FOUND AT AFT CARGO COMPARTMENT FROM FR57 TO FR59 AT S-42RH AND BETWEEN 260MM AFT FR57 AND 200MM FWD FR57 AT S-43L WITH CORROSION. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL.. AND FINAL APPROVAL AND FINAL APPROVAL UNDER AIRBUS DOSSIER 81042127 AND COOPESA'S ENGINEERING ORDER COO-EO-2022-15280 .