As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN METAL FLOOR PANEL 102C HAS CORROSION AROUND FASTENER HOLES, 2EA HAT CHANNELS CRACKED AND END SKIN TORN. REMOVED CORROSION IAW SRM 53-01 FIG 1 ORIGINAL MATERIAL .032" REMOVED .002 FOUND TO BE WITHIN LIMITS IAW SRM 53-01 FIG 1. REMOVED DAMAGED AREAS OF 3EA HAT CHANNELS AND SKIN PANEL IAW SRM 53-05. INSTALLED HAT CHANNELS AND SPLICES IAW SRM 51-30-02. INSTALLED FILLER AND DOUBLER IAW SRM 53-05 FIG 1 P226.