As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGE WAS DISCOVERED ON THE TAIL BOOM LOWER SKIN (PN: 350A23-4288-20) AT THE UPPER AFT AREA OF THE BATTERY DOOR OPENING. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC130-53-2024-2929, ISSUE A DATED 23 SEP 2024.