As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN HAD BULGE WITH RIVETS PULLING AT REINFORCING DOUBLER FOR FWD LAV SERVICE PAN, STA 424-434 LBL 5 APPROX. CUT OUT DAMAGED SECTION OF SKIN AND INSTALLED REPAIR DOUBLER AND STRUCTURAL FILLER REF ECRA5331-01397 AND DIPPED TO PERFORM A PERMANENT REPAIR PER PART 3 WITHIN 12 MONTHS. 53-DIP CONTROL NUMBER 871501.