As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT RIGHT SIDE FUSELAGE SKIN BETWEEN FRAMES 16A TO 18 AND BETWEEN STRINGERS 41 AND 43 RT MEASURES 11 INCH BY 8.1. "REPAIR NOT IAW WITH SRM 53-12-12 FIG 201, REPAIR NOT APPLICABLE TO AREA. REMOVED AND REPLACED REPAIR IAW EA 6-5310-118112. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION.