What was found
DOT A24-8 MID CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 STEPS 3A; C-F<BR>VERIFIED REPAIR MATERIALS AS GLASS FABRIC--BMS9-3 (A164924); RESIN--EPOCAST 50A1 (A176810) IAW SRM 53-00-50-2R-1 TABLE 201<BR>NEED OK TO BOND;[02] VERIFIED ITEM 1<BR>OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEPS 3J-M. TAP TEST GOOD.;[04] REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD 241AF IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD.;[05] VERIFIED ITEMS 3 AND 4;[06] AUDIT C/W