What was found
DOT 114-025. CABIN FLOORBOARD 231XF UPPER SURFACE HAS AREAS OF PULLED FIBERS.<[01] BONDTEST IAW B737 NDT PART 4; 51-00-05. NO DEFECTS NOTED. TOOL#40082; DUE 10OCT23<BR>UT IAW B737 NDT PART 4; 51-00-03. NO DEFECTS NOTED. TOOL#40084; DUE 01AUG24. REF STEP 2 OF EA 23-153-02916-WIP1;[02] EVALUATED PANEL 231XF AND FOUND AREA OF PULLED FIBERS AND DENTS 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 5-28 (A201245); BMS 8-201 (A201552); BMS 9-3 (A190974). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. APPLIED POTTING COMPOUND. IAW B737-700 SRM 53-00-50-2R-1 PAR 3 H-J. NEED OK TO BOND.;[03] VERIFIED STEP 2;[04] OK TO BOND;[05] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR3 K-M.;[06] REPAIRED UPPER SURFACE ON PANEL 231XF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[07] REFER TO FAULT TTG8Q00NMDKV WHERE EA 23-153-02916 WAS ADDED AS A SUBTASK;[08] VERIFIED ITEM 5; 6 AND 7.<BR>TAP TEST GOOD REF NDT PART 1 51-01-01 REPAIR INSPECTION FLOWCHART FIGURE 9. AAR TOOL 35009;[09] AUDIT C/W