What was found
SUPPLEMENTAL INFORMATION AFT PASSENGER CABIN FLOOR PANEL 242TF UPPER SURFACE COMPOSITE PLY DAMAGED 13" FROM FORWARD END AND 14-24" FROM INBOARD EDGE, (BETWEEN BS. 887 TO BS. 1016). REPAIRED PANEL IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUPPLEMENTAL INFORMATION AFT PASSENGER CABIN FLOOR PANEL 242TF UPPER SURFACE COMPOSITE PLY DAMAGED 13" FROM FORWARD END AND 14-24" FROM INBOARD EDGE, (BETWEEN BS. 887 TO BS. 1016). REPAIRED PANEL IAW SRM.