What was found
PASSENGER CABIN FLOOR PANEL 232SF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL DOWN THE CENTER. DOT 203-30 / [01] EVALUATED PANEL 232SF AND FOUND AREA'S OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201 (A141867); BMS 9-3 (A10269; BMS 5-28 (A125915). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 K-M. CURED AT 150 DEGREES (AAR 30347 EXP 4-30-23). TAP TEST GOOD.;[04] REPAIRED PASSENGER CABIN FLOOR PANEL 232SF TOP SIDE LENGTH OF PANEL DOWN THE CENTER IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4