As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGE TO THE CABIN FLOOR RH SPAR / EDGE FRAME (PN: 350A21-1600.20) WAS IDENTIFIED AT TWO LOCATIONS BENEATH THE RH FITTING AT APPROXIMATELY FS 64” MEASURING APPROXIMATELY 1.00” AND 0.60”. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET RDAS-EC130-53-2023-2501, ISSUE A DATED 18 AUG 2023.