As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A 1000 HR. INSPECTION, THE RH SIDE OF FRAME 7 IN THE TAIL CONE IS DAMAGED IN THE FORM OF A CRACK. THE CRACK IS LOCATED IN THE BEND RADIUS OF THE FLANGE NEAR THE LOWER RH OMEGA STRINGER AND IS REPORTED TO BE APPROXIMATELY 0.35 LONG. A DETAILED DESCRIPTION OF THE DAMAGE AND AN APPROVED REPAIR PROCEDURE IS PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC135-53-2025-3789, REV A DATED 23 NOV 2025.