What was found
DOT A-24-1 MID CABIN FLOOR PANEL 241BF HAS PULLED FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E; AND F. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; RESIN EPOCAST 50A (A137343; FIBERGLASS CLOTH BMS 9-3 (A10269). <BR><BR>REQUIRES OKAY TO BOND REPAIR.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS J;K;L; AND M. CURED AT 150 DEGREES THERMOMETER AAR30347 CAL DUE 4/30/23. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 241BF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1 PAR 3.;[05] VERIFIED STEPS 3-4