As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EVALUATION FOR POSSIBLE FCS REPAIR ON UPPER SKIN ON TAIL ON FRAME 83 BETWEEN STRINGER 4L TO STRINGER 5L, REMOVED AND REINSTALLED EXISTING REPAIR LOCATED ON TAIL ON FRAME 82 AND BTW STR 4L TO STR 5L AS PER ER/A 549159-14 REV. A AND A320 SRM 53-51-11 FIGURE 203.