What was found
DOT A-24-8 CENTER CABIN FLOOR BOARD 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-2 PAR 3 STEPS A;C;E;F; AND I. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-2 TABLE 201; RESIN EPOCAST 50A (A145898); FIBERGLASS CLOTH BMS 9-3 (A10269).<BR><BR>REQUIRES OKAY TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 REPAIR 1 PAR 3 STEPS K;L;AND M. TAP TEST GOOD.;[04] REPAIRED CENTER CABIN FLOOR BOARD 241AF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1.;[05] VERIFIED STEPS 3-4