What was found
MAIN CABIN FLOOR PANEL NR 32 IS CRACKED AT FWD END AT FASTENER HOLE. CUT OUT DAMAGE SECTION FABRICATED DOUBLER & FILLER AND INSTALLED IAW SRM 51-30-02, 53-05, FIG 1. TREATED & PRIMED IAW SRM 51-10-3. REQUIRED INSPECTION COMPLETED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FLOOR PANEL NR 32 IS CRACKED AT FWD END AT FASTENER HOLE. CUT OUT DAMAGE SECTION FABRICATED DOUBLER & FILLER AND INSTALLED IAW SRM 51-30-02, 53-05, FIG 1. TREATED & PRIMED IAW SRM 51-10-3. REQUIRED INSPECTION COMPLETED.