What was found
PASSENGER CABIN FLOOR PANEL 242AF TOP SIDE HAS PULLED FIBERS THE LENGTH OF THE PANEL 2' INBD OF R/H SIDE. DOT 203-23 / [01] EVALUATED DAMAGE TO FLOOR PANEL 242AF FOUND WITH-IN REPAIRABLE LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SUFACE OF FLOOR PANEL 242AF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-J);[03] VERIFIED MATIERIALS FOR WET LAY-UP TO UPPER SURFACE OF FLOOR PANEL 242AF IAW B737-700 SRM 53-00-50-2R-1 REAIR 1 TABLE 201<BR><BR>RESIN BMS 8-201 TY III (A137346)<BR><BR>FABRIC BMS9-3 TY H3 (A13436)<BR><BR>POTTING COMPOUND BMS 5-28 TY 19 (A133227);[04] OK TO BOND REPAIR PLIED TO UPPER SURFACE OF FLOOR PANEL 242AF;[05] VERIFIED STEPS 1; 2; AND 3 C/W;[06] OK GIVEN TO BOND REPAIR;[07] BONDED REPAIR PLIES TO UPPER SURFACE OF FLOOR PANEL 242AF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (K-O)<BR><BR>REPAIR COMPLETE;[08] VERIFIED STEP 7 C/W;[09] JOB COMPLETED; AUDIT C/W