As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BULGED FUSELAGE SKIN PANEL AT BS 1030 JUST BELOW RIGHT AFT SERVICE DOOR LOWER HINGE. REMOVED AND REPLACED SKIN PANEL 8 BY 8. REMOVED SURFACE CORROSION FROM SKIN AT LAP SEAM (.002) AND PRESSURE STOP FITTING, O/B SIDE APPROX .022, WITHIN LIMITS PER SRM 53-10-1.