What was found
CRACKED CHANNEL OF FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131B, AND SRM 51-70-1D PAR 10. HFEC INSPECTION WAS ACCOMPLISHED NO CRACKS FOUND AFTER STOP DRILL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED CHANNEL OF FLOOR PANEL. FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131B, AND SRM 51-70-1D PAR 10. HFEC INSPECTION WAS ACCOMPLISHED NO CRACKS FOUND AFTER STOP DRILL.