As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EMPENNAGE FRAME 84 AT STRINGER 13 L, THE FRAME LOWER CHORD IS CORRODED AT AND UNDER THE CROSSBEAM. REMOVED CORROSION FROM THE FRAME FLANGE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00, FIG 105 AND TABLE 102. REMOVED THE FLANGE IAW SRM 51-40-21. FABRICATED A NEW FLANGE CHORD IAW AIRBUS DWG A53988401. ALODINED IAW SRM 51-21-10. PRIMED AND IAW SRM 51-23-10. INSTALLED FLANGE IAW SRM 51-40-21.