As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION IN SEVERAL PLACES, BS 1640 LBL 65 BL 0 WL 208 FLOORBEAM. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AT BS 1640 LBL 14, 31, AND 56 IAW B757-200 SRM 51-10-02 ORG MAT THICKNESS IS .125 MAX REMOVED IS .011 AND IS WITHIN LIMITS IAW B757-200 SRM 53-00-51 FIG 101. REMOVED CORROSION AT BS 1640 LBL 9 IAW B757 -200 892477.