As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND ON BS 947 FLOOR BEAM; LBL 24; WL 208; AFT EDGE OF THE UPPER CHORD.<[01] CORROSION ON BS 947 FLOOR BEAM; LBL 24; WL 208; AFT EDGE OF THE UPPER CHORD ORIGINAL MATERIAL THICKNESS IS .180' LOWEST MATERIAL REMAINING IS 0.140' FOUND TO BE OUT OF LIMITS; IAW SRM 53-70-51-1A-1 DISCREPANCY TO BE REPAIRED ON COSTUMER CARD TTG8Q00K38HP;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.