What was found
DURING INSPECTION, FOUND FORWARD CABIN FLOOR PANEL 222FF DAMAGE AND PUNCTURED. DAMAGED DIM: L=3" W=2" D=.020" NO ESTABLISH LIMIT ON SRM. REPLACED FLOOR PANEL, IAW SRM 5 1-72-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND FORWARD CABIN FLOOR PANEL 222FF DAMAGE AND PUNCTURED. DAMAGED DIM: L=3" W=2" D=.020" NO ESTABLISH LIMIT ON SRM. REPLACED FLOOR PANEL, IAW SRM 5 1-72-11.