As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION SPOTS ON FUSELAGE SKIN PANEL AT C39, P55 LT (P/N SPLICE A538-12119-200, SKIN PANEL A538-10775-200). REPAIR PERFORMED BY BLEND OUT THE CORROSION AND INSTALLING OVERSIZE FASTENER IAW EA 6-5315-106500 AND RAS 053011/010/2007 ISS A.