As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION ON FUSELAGE SKIN RUNNING UNDERLAP SEAM AT STRINGER 14R FROM BS 781 TO 800 & ON BUTT STRAP SURFACE INSIDE BUTT JOINT AT BS 781. REQUIRING ADDITIONAL STRIPPING FROM BS 781 TO 900. ACCOMPLISHED EA F-5330-T0309546 FUSELAGE PLATES & SKINS LOWER SKIN PANEL CORROSION REPAIR AT LAP JOINT STATION 781 TO 900 STRINGER 14R. CATEGORY B MAJOR REPAIR.