As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND THE FORWARD FUSELAGE CARGO FLOOR SUPPORT CORRODED AND A CRACK ON UPPER FLANGE AT BS 643, RBL 20.5. THE CRACKED AREA OF FLOOR SUPPORT WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-40-5. (M)