As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORRODED ON RADOME UPPER BRACKET AT 12 OCLOCK POSITION ON INTERNAL SIDE AT AFT END STA 199, RBL 3 AREA .75 X .75. REMOVED CORROSION FROM RADOME BRACKET ORIGINAL THICK .075. MATERIAL REMOVED .003 FOUND TO BE WITHIN LIMITS SRM. TREATED AND PRIMED. (K)