As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CABIN FLOOR PANEL 242AF HAS DAMAGED UPPER PLYS. EVALUATED DAMAGE TO UPPER PLIES; DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-1. TAP TESTED GOOD, NO DELAMINATION NOTED. CLEANED & PREPPED REPAIR AREA IAW SRM 53-00-50-2R-1 PAR 3; STEPS A;C;E;F;I; AND J. BONDED REPAIR PLIES IAW SRM 53-00-50-2R-1 PAR 3; STEPS K;L; AND M. TAP TESTED GOOD. REPAIRED CABIN FLOOR PANEL 242AF UPPER SURFACE IAW SRM 53-00-50-2R-1 PAR 3.