What was found
DOT A24-9 MID CABIN FLOOR PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE TO UPPER AND LOWER SUFACES TO BE REPAIRABLE IAW SRM 53-00-50-2R-2 TABLE 201 REPAIR 2<BR>CLEANED AND PREPPED UPPER AND LOWER SURFACE IAW SRM 53-00-50-2R-2 STEPS 3A;C-F<BR>APPLIED POTTING COMPOUND IAW SRM 53-00-50-2R-2 STEPS 3F-3I. POTTING COMPOUND-- EPOCAST1619 (A181386)<BR>VERIFIED BOND MATERIALS AS-- GLASS FIBER- BMS9-3 (A164924); RESIN- EPOCAST 50A1 (A178557) IAW SRM 53-00-50-2R-2 TABLE 201<BR>NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-2.PAR 3J-L. AAR OVEN BO-06 D.D. 7-27-23. 150DEG 2HRS.;[04] REPAIRED DAMAGE ON PANEL 232 RF. IAW B737-700 SRM 53-00-50-2R-2; SRM 53-00-50-2R-0.;[05] VERIFIED ITEMS 3 AND 4<BR>AUDIT C/W