As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(DOT 38-24) RH LOWER FUSELAGE SKIN CORRODED STA 1788 APPROX 4" AREA, 3" ABOVE THE APU RH DOOR CUTOUT. COMPLIED WITH REPAIR ON EA F-5330-T0382463 P1 FUSELAGE-PLATES & SKINS-SKIN REPAIRS AT STA 1885 RHS AND STRINGER S-17R FOR CORROSION MAJOR REPAIR