What was found
CRACK ON FLOOR PANEL 200F. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05, FIG 131B, PAR 145.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FLOOR PANEL 200F. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-05, FIG 131B, PAR 145.