As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION IN BOLT HOLES, BS 1640, BL 0 TO RBL 64 WL 208. REMOVED CORROSION AT BOLT HOLES FLOORBEAM BS 1640 RBL 64 WL 208 IAW B757-200 SRM 51-10-02-0G PAR 14 FIG 1. ORG MAT THICKNESS IS .125.MAT REMAINING IS .094. MAT REMOVED IS .031 AND IS OUT OF LIMITS IAW B757-200 SRM 53-00-51 DETAIL VI. REPAIRED BS 1640 RBL 64 WL 208 IAW ECRA 5310-05536.