As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C-CHECK - DURING INSP FOUND CORROSION ON ATTACHMENT ANGLE 26R FWD OF THE AVIONICS DOOR. REMOVED ATTACHMENT ANGLE IAW SRM 51-42-06-001-001-A01, STARTED BLENDING CORROSION, AFTER BLENDING FOUND BLEND TO BE BEYOND LIMITS IAW SRM 53-21-23-101-003-A01. LOCATED FASTNER HOLES IN NEW ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE IAW SRM 51-42-21-001-001-A01. TOPCOATED IAW SRM 51-25-16-001-001-A01, APPLIED CORROSION INHIBITING COMPOUND IAW 51-21-11-001-001-A01.