As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE TOILET SERVICE DOOR PAN, AFT LOWER CORNER IS BUCKLED. REMOVED FUSELAGE TOILET SERVICE DOOR PAN IAW SRM 51-40-02. AFTER REMOVAL OF FUSELAGE TOILET SERVICE DOOR PAN FOUND CORROSION ON THE MATING SKIN OF SERVICE DOOR PAN. REMOVED CORROSION IAW SRM 53-00-01. PERFORMED THICKNESS TEST PER NDT PART 4 51-00-00, PROCEDURE 2. FOUND DEEPEST POINT OF BLENDED SKIN TO BE .057. INSTALLED THE LAV SERVICE DOOR PAN IAW SRM 51-40-02.