As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CARGO DECK FLOORBEAM UPPER CHORD CORRODED BS 1040-BS 1080 RBL 26. CORROSION REMOVED IAW SRM 51-10-02 REV 125 AND FOUND TO BE OUT OF LIMITS IAW SRM53-00-51-1A DETAIL III REV 125. NOMINAL THICKNESS OF UPPER CHORD 0.090" MAX ALLOWABLE BLEND=10%=0.009 ACTUAL MAX BLEND DEPTH= 0.024". FLOORBEAM UPPER CHORD REPLACED IAW DWG 144N8017, 111N5201 AND SRM 51-40-02 REV 125 BETWEEN BS1040 TO BS 1080.