As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C&SI, CORROSION ON INTERNAL SIDE OF NLG LT SIDE WALL AT BS 285 (FWD OF VERTICAL STIFFENER) LWR END CORROSION FOUND AT BS 280 & 285 BETWEEN STIFFENER AND SKIN. SKIN CUTOUT MADE AT VERT STIFFENER TO REMOVE CORROSION IAW SRM 51-10-6. DOUBLER FABRICATED IAW SRM 51-40-2. FILLERS FABRICATED IAW SRM 51-40-2. INSTALLED IAW SRM 51-40-2.