As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLOOR PANEL SUPPORT UPPER SURFACE IS CORRODED AT FASTENER HOLE BS 1653-BS 1658, LBL 54. REMOVED CORROSION AS REQUIRED, IAW B757 SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .071 MATERIAL LOSS OF .002 REMAINING MATERIAL THICKNESS .069. FOUND TO BE WITHIN LIMITS, IAW BOEING DRAWING 657N47303 REV B AND B757 SRM 53-60-15-1A DETAIL IV. RESTORED FINISH, IAW B757 SRM 51-20-01-04.