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