As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, DAMAGE WAS DISCOVERED TO THE COCKPIT FLOOR UPPER SKIN PANEL (P/N: L533M1014217) IN THE FORM OF MULTIPLE DENTS AND DEBONDED SKIN. THE DENTED AND DEBONDED AREAS ARE REPORTED TO BE FROM 0.50” X 0.50” IN SIZE TO 4.0” X 4.0” IN SIZE. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2025-3327A, REV A DATED 17 OCT 2025.