As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MID CABIN FLOOR PANEL 231ZF HAS PULLED FIBERS ON UPPER SURFACE. EVALUATED & FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A, C, E, & F. BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. TAP TESTED GOOD. REPAIRED MID CABIN FLOOR PANEL 231ZF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.