As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN, FWD R/H WET AREA, FLOOR BAEM CORRODED AT NUT PLATES STA 325 RBL 35-58 REMOVED CORROSION ORIGINAL THICKNESS .120 REMOVED .011 NEW THICKNESS .109 WICH IS FOUND TO BE WITHIN LIMITS WICH IS FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-10-08-1A AND BOEING DWG 141N2930 APPLIED ALODINE, PRIME AND TOP COAT IAW B757 SRM 51-20-01- 0G