As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE TO THE RIGHT-SIDE EDGE FRAME / SPAR (PN: 350A21-1600.20) IN THE FORM A CRACK AT APPROXIMATELY FUSELAGE STATION 34” WAS DISCOVERED. THE DAMAGED AREA OF THE EDGE FRAME WAS REMOVED, AND A NEW EDGE FRAME WAS SPLICED IN FOLLOWING THE GENERIC APPROVED REPAIR PROCEDURES PROVIDED IN AIRBUS REPAIR DESIGN APPROVAL SHEET AHI-130-53-003-21, REVISION A DATED 15 JAN 2021.