What was found
CRACK ON FLOOR PANEL. FLOOR PANEL WAS REPAIRED IAW SRM 51-70-1-D, PAR 10, AND SRM 53-05, FIG 131-B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FLOOR PANEL. FLOOR PANEL WAS REPAIRED IAW SRM 51-70-1-D, PAR 10, AND SRM 53-05, FIG 131-B.