What was found
A24-32 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALED FLOOR PANEL 242AF UPPER SURFACE. FOUND WITH-IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 242AF UPPER SURFACE FOR WET LAY-UP REPAIR IAW B737-700 SRM 53-00-50-2R-1 STEPS 3(A-J);[03] VERIFIED MATERIALS FOR REPAIRS TO FLOOR PANEL 242AF IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 TABLE 201 <BR><BR>POTTING COMPOUND BMS 5-28 TY 19 (A153169) <BR>RESIN BMS 8-201 TY IV (A161394) <BR>FABRIC BMS 9-3 TY H3 (A94417);[04] VERIFIED STEPS 1; 2 & 3;[05] OK GIVEN TO BOND;[06] 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>REPAIR COMPLETE;[07] VERIFIED STEP 6;[08] VERIFIED JOB COMPLETE; AUDIT C/W