What was found
DOT A-24-1 MID CABIN FLOOR PANEL 242AF HAS PULLED FIBERS ON UPPER SURFACE. / [01] EVALUATED PANEL 242AF AND FOUND AREA OF 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 PAR 3A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201 (A137335); BMS 9-3 (A24484). NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES. IAW B737-700 SRM 53-00-50-2R-1 PAR 3K-M. AAR DIGITAL THERMOMETER 30347 150DEG 2HRS.;[04] REPAIRED AREA OF PULLED FIBERS ON UPPER SURFACE ON PANEL 242AF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4