As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 1183 - 1148 OB AND STR 26L HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2 AND 53-30-2 FIG 2. REPAIRED SKIN IAW EA NR 7-5330-126867 FUSELAGE SKIN AD 98-11-03 R1, STA 1152 STA 1175 STR 26L 65-54583 LAP JOINT UPPER AND LOWER SKINS CORROSION REPAIR.