What was found
DOT A24-23 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] FABRICATED NEW BOARD FROM SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4; BOEING DRW. 144A5810 AND BAC5085 STEP 8.4.2.<BR>CURED ADHESIVE WITH HEAT LAMP AND DIGITAL THERMOMETER 30347 DUE 5-8-24<BR>FLOOR STOCK (WN13845); INSERTS (A194295); ADHESIVE (A191086);[02] VERIFIED STEP 1;[03] INSTALLED MARKINGS ON FLOOR PNL 242AF IAW DRW 144A5810 AND 144A5810-189;[04] VERIFIED STEP 3<BR>AUDIT CW