What was found
DOT A-24-04. MID CABIN FLOOR PANEL 232SF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [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 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 (A137335); FIBERGLASS CLOTH BMS9-3 (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; AND M. CURED AT 150 DEGREES; THERMOMETER AAR30347; CAL DUE 4/30/23. TAP TEST GOOD.;[04] REPAIRED CABIN FLOOR PANEL 232SF TOP SIDE IAW B737 SRM 53-00-50-2R-1; PAR 3.;[05] VERIFIED STEPS 3-4