What was found
DOT A24-6 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C-F. <BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A176065); FABRIC (A164924);<BR><BR>REQUEST OK TO BOND;[02] VERIFIED ITEM 1<BR>OK TO BOND;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 J-M. TAP TEST GOOD.;[04] REPAIRED MID CABIN FLOOR PANEL 242AF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4