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 CONE SKIN (PN: L533M1022262) ON THE RH SIDE. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2024-1344, ISSUE A DATED 06 MAY 2024.