As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE AFT BOTTOM OUTER SKIN HAS SEVERAL CORRODED FASTENERS FROM BS 559+80 TO 559+112, STRINGER 27. REMOVED THE CORROSION FROM THE EXTERNAL SKIN IAW SRM 51-21-06. ORIGINAL MATERIAL THICKNESS .058", MINIMUM MATERIAL REMAINING .051", MAX MATERIAL REMOVED .007", MAX ALLOWABLE .006". FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM AND SRM . COMPLIED WITH REO