What was found
DOT A24-4 MID CABIN FLOOR PANEL 241AF HAS MULTIPLE PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT 4; 51-00-03. NO DEFECTS NOTED. TOOL#36285; DUE 16DEC23. REF EA 23-153-02790-WIP1 STEP 2;[02] EVALUATED PANEL 241AF 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 3 A; C; E&F. VERIFIED MATERIALS AS: BMS 8-201 (A197641); BMS 9-3 (A178073). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[03] VERIFIED STEP 1 AND 2 C/W AND OK TO BOND GRANTED;[04] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 K-M.;[05] REPAIRED DAMAGE TO UPPER SURFACE ON PANEL 241AF. IAW B737-700 53-00-50-2R-1; SRM 53-00-50-2R-0& EA 23-153-02790.;[06] VERIFIED STEPS 4-5.<BR>AUDIT C/W.