As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C RIGHT BLG W/W TOP PANEL SUPPORT STIFFENER SURFACE CORROSION REVEALED AT STA 1403 RBL 96-98. CORROSION BLEND OUT 0.033 X 2 X 4 INCH EXCEED SRM 53-10-01 FIG 1 LIMIT. SUPPORT STIFFENER REPAIRED AS PER SRM 51-40-04 FIG 1.