As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK DAMAGE WAS NOTED TO THE LEFT SIDE AFT BOX BEAM INNER SKIN PANEL (PN: B533K5606-212) MEASURED TO BE APPROXIMATELY 0.625” LONG. THE DAMAGE WAS REPAIRED VIA A REPAIR DOUBLER IN ACCORDANCE WITH AIRBUS RDAS-BK117-53-2021-4226, REVISION B DATED 02 DEC 2021.