What was found
DOT A24-8 CENTER CABIN FLOOR BOARD 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE ON UPPER SURFACE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1 PARA 1A. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A C E-F. VERIFIED MATERIAL BMS 9-3 (A162523) BMS 8-201 (A172533) IAW SRM 53-00-50-2R-1 TABLE 201. <BR><BR>NEED OK TO BOND;[02] VERIFIED STEP 1<BR>OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR3 K-M. TAP TEST GOOD.;[04] REPAIRED DAMAGE ON UPPER SURFACE OF PANEL 241AF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4