What was found
DOT A24-8 MID CABIN FLOOR PANEL 231YF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE.<[01] EVALUATED PANEL 231YF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR3A;C;E&F. VERIFY MATERIAL AS: BMS 9-3 (A150508); BMS 8-201 (A153126). NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-0 PAR 3K-M.AAR OVEN BO-06 2-4-23 150DEG 3HRS.;[04] REPAIRED UPPER SURFACE ON PANEL 231YF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0;[05] VERIFIED STEPS 3-4