What was found
DOT A-24-4 CENTER CABIN FLOOR BOARD PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A; B; C; E; F; AND J. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201 RESIN EPOCAST 50A; (A141867); FIBERGLASS CLOTH BMS 9-3 (A10269). <BR><BR>REQUIRES OKAY TO BOND REPAIR PLIES.;[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; M; AND N. OVEN B0-06 CAL DUE 11/8/22. TAP TEST GOOD.;[04] REPAIRED CENTER CABIN FLOOR BOARD PANEL 241AF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 REPAIR 1.;[05] VERIFIED STEPS 3-4