What was found
CRACK ON CABIN FLOOR PANEL 256A. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-10-3, PAR 14 AND 21 AND SRM 53-01, FIG 4, SHEET 4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON CABIN FLOOR PANEL 256A. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-10-3, PAR 14 AND 21 AND SRM 53-01, FIG 4, SHEET 4.