As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HN00147837 DISCREPANCY: FUSELAGE OUTER SKIN IS CHAFED UNDER AFT LAV. RINSE/FILL PORT. CORRECTIVE ACTION: FOUND AN EXTERNAL REINFORCING DOUBLER AROUND CANNON PLUG PL118J1 TO BE CHAFED. NOT THE EXTERNAL SKIN. COMPLIED WITH REMAINING STEPS OF REO 670-53-51-281 REV - DATED 2024-04-05