As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE LWR BODY AT PANEL CUTOUT BTW STA 277 AND STA 351 CORROSION SKIN AND NUTPLATES. REMOVED NUTPLATES AND CORROSION IAW SRM 51-10-6 AND 51-30-2 AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG1. REMOVED T-ANGLE AND FABRICATED NEW T-ANGLE IAW DWG NR 65-10936. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED NEW T-ANGLE AT LOWER FUSELAGE STA 351 IAW SRM 51-30-2 AND MFG DRAWING NR 65-10936.