What was found
CABIN FLOOR PANEL 222AF HAS UPPER SURFACE FIBER DAMAGE. / UPPER SURFACE FIBER DAMAGE TO CABIN FLOOR PANEL 222AF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1; AND SRM 53-00-50-2R-4. 59198U 3.20.20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CABIN FLOOR PANEL 222AF HAS UPPER SURFACE FIBER DAMAGE. / UPPER SURFACE FIBER DAMAGE TO CABIN FLOOR PANEL 222AF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1; AND SRM 53-00-50-2R-4. 59198U 3.20.20.