As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A 1000 HOUR AIRFRAME INSPECTION FOUND L/H KEEL BEAM CAP P/N L533M1009203 AND R/H KEEL BEAM CAP P/N L533M1010203 CORRODED AT THE END OF THE CAP ON BOTH SIDES. THE CORROSION IS THROUGH THE FULL THICKNESS OF THE CAP. PERFORMING A REPAIR AS PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2023-2832