As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FLOORBEAM CORRODED AT STA 1030, LBL 19, WL 208, UPPER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REF FED EX PF SRM 53-10-1 PG 26 AND 38. ORIGINAL THICKNESS IS .125" MATERIAL REMOVED IS .030" MAT. REMAINING IS .095'. INSTALLED REPAIR ANGLE AND FILLER REF FED EX SRZ 53-034 REF REPAIR NR 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.