As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 AFTER REMOVAL OF C-2 (B-PIT) SCUFF PLATE FOUND CORROSION ON FUSELAGE SKIN. REMOVED CORROSION AND FOUND SKIN TO BE OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. PROCURED AND INSTALLED REPLACEMENT SKIN FROM STA 450-610 L31L-L31R IAW SRM 51-1-20D, AND SRM 51-1-21.