As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION SPOT ON AFT CABIN WET AREA FLOORBEAM UPPER FLANGE AT BS 986.5 R.BL. 5'. REMOVED CORROSION IAW SRM 53-70-51-1A-1-A00108. PERFORMED UT THICKNESS INSP. IAW NDT PART 4; 51-00-00; PROCEDURE 3. MIN. THICKNESS 0.137'. FOUND TO BE OUT OF LIMITS IAW SRM=53-70-51-11A-1. REPAIR ACCOMPLISH ON TASK CARD TTG8Q00A436K.