As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN FLOOR PANEL 232 UG IS CRACKED AND DAMAGED. FABBED A NEW FLOOR PANEL 232 UG BY USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED THE PANEL IAW FEDEX DWG SRZ 25-005, REV F.