As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AROUND FWD LAV SERVICE PANEL. FWD LAV SERVICE PANEL AFT INBD CORNER SEPARATED FROM FUSELAGE. INSPECTED INTERIOR AND FOUND INTERNAL STRUCTURE OF SERVICE PANEL CORRODED. NDT ON EXTERNAL SKIN SHOWS EXCESSIVE MAT LOSS DUE TO CORR RMVL. MAPPING AREA TO FORWARD TO EG. HAVE NEW PAN, MFG'G CLIPS TO INSTALL. REPAIRED IAW C7 TO WU L0364H.