As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 1000 HOUR INSPECTION, CHAFE DAMAGE WAS DISCOVERED ON THE FRAME 4 INNER SKIN PANEL (PN: L533M1407205). A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE WAS COMPLIED WITH PER AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-3666, ISSUE A DATED 21 NOV 2024.