What was found
CABIN FLOOR PANEL 231YF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231YF IAW SRM 53-00-50-2R-1, REPAIR 1 STEPS 3, (K-O).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CABIN FLOOR PANEL 231YF UPPER SURFACE HAS PULLED FIBERS. FOUND WITHIN REPAIRABLE LIMITS IAW SRM 53-00-50-2R-1, REPAIR 1. BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 231YF IAW SRM 53-00-50-2R-1, REPAIR 1 STEPS 3, (K-O).