As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN LAV VAC OUTLET CUT-OUT CORRODED. ACFT GROUNDED. REMOVED CORROSION AROUND LAV VAC OUTLET CUTOUT IAW SRM 53-00-01-1A-1. ORIG THICKNESS .125, REMOVED .015 REMAINING THICKNESS .111. FOUND TO BE WITHIN LIMITS. AREA IS 1.95 BY .95. TOOL USED T8225P RESORTED TOP COAT IAW AMM 51-21-99.