What was found
DOT A-24-24 CENTER CABIN FLOOR PANEL 241CF HAS PULLED COMPOSITE FIBER DAMAGE ON UPPER SURFACE. / [01] EVALUATED DAMAGE; UPPER SURFACE FOUND TO BE REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A; C;E;F;G;H;I; AND J. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A10269); RESIN EPOCAST 50A (A147728); POTTING COMPOUND EPOCAST1619 (A125915). <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 PAR 3 STEPS K;L; AND M; CURED AT 150 DEGREES; OVEN B0-06 CAL DUE 11/8/22. TAP TEST GOOD.;[04] REPAIRED UPPER SURFACE OF CABIN FLOOR PANEL 241CF IAW B737 SRM 53-00-50-2R-1.;[05] VERIFIED STEPS 3-4