What was found
DOT A-24-07 CENTER CABIN FLOOR PANEL 232SF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[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 1. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 A;C;E&F. VERIFY MATERIALS : BMS 8-201 (A153219); BMS 9-3 (A150508). IAW B 737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO PAINT.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M.;[04] REPAIRED AREA'S OF PULLED FIBERS ON UPPER SURFACE OF PANEL 232SF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4