As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AIRCRAFT DAMAGE ON AFT FUSELAGE BETWEEN FRAMES 65 AND 66 JUST BELOW STRINGER 36. REPAIRED FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 36 IAW SRM 53-10-10 FIG 749. EDDY CURRENT INSPECTION IAW AIRBUS NDT MANUAL PART I 51-30-00. NO CRACK INDICATION FOUND, WORK ACCOMPLISHED ON ASTAR N/R 014897 AND 014898 AND LOG BOOK PAGE 093482 ITEM 4M.