As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT THS REAR SPAR UPPER TEE CAP UPPER SURFACE HAS CORROSION BETWEEN RIB 14 - 15. REMOVED CORROSION IAW A300-600 SRM 51-74-10. ORIG THICKNESS .080 IAW AIRBUS DWG A55177703. MAT REMAINING .054. FOUND AREA TO BE OUT OF LIMITS IAW A300-600 SRM 55-10-00 PG 106 TOOL: T8225T, REPAIRED AREA IAW A300-600 SRM 55-11-21 FIG 212.