What was found
AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT 241AEF SURFACE SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FLOOR PANEL 241AEF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT 241AEF SURFACE SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.