What was found
DOT A-24-1 MID CABIN FLOOR PANEL 231XF HAS PULLED FIBERS ON UPPER SURFACE. EVALUATED PANEL 231XF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW 53-00-50-2R-1 PAR 3 A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201 (A137335); BMS 9-3 (A24484). NEED OK TO BOND. BONDED REPAIR PLIES. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M. REPAIRED AREA OF PULLED FIBERS ON UPPER SURFACE ON PANEL 231XF. IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.