As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING 800 HOUR INSPECTION, DAMAGE TO THE FORWARD BOTTOM FRAME 1 IN THE FORM OF A CRACK WAS DISCOVERED AT LBL 195MM AND IS APPROXIMATELY 1.2” IN LENGTH. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-BK117-53-2024-3340.