As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE MAIN CARGO CABIN FROM BS 1130 TO BS 1183 BETWEEN LBL 25 AND LBL62 FLOOR WEB WITH DOUBLE HOLES AND CORROSION. REMOVED CORROSION FROM BS 1130 TO BS 1154.75 BETWEEN LBL 25 AND LBL 31 AND FROM BS 1154.75 TO BS 1183 BTWN LBL 25 AND LBL 62 FOUND WITHIN LIMITS IAW SRM 53-10-1 FIG 1. REPAIRED FLOOR WEB FROM BS 1130 TO BS 1154.75 BETWEEN LBL 31 AND LBL 70 IAW SRM 51-40-2 FIG 1.