As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE - ZONE 312 - UPPER AFT R/H FUSELAGE APROXIMATE STA 2163 TO 2092, STRINGER 11R TO 13R CORROSION PRESENT. AFT FUSELAGE ZONE 312 UPPER AFT R/H FUSELAGE STA 2163.685 TO 2069.440, STRINGER 11R TO 13R CORROSION REPAIR PERFORMED IAW EA 1-5330-T0365138 PART 1 " FUSELAGE-PLATES & SKINS- FUSELAGE AFT BODY SECTION-SKIN PANEL AJC7058-2 - REPAIR" *MAJOR REPAIR* SEE JPF.