What was found
PASSENGER CABIN FLOOR PANEL 241AF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 SECTION 44. <BR>CABIN FLOOR UPPER SURFACE EXCEEDS ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4 CONDITIONS A-F REQUIRES REPLACEMENT.<BR>FABRICATE REPLACEMENT FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] BEGAN FABRICATING NEW FLOOR PANEL 241AF USING BMS 4-23 LOT#1508290-1 IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE).;[03] COMPLETED FABRICATION OF NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1.A(NOTE).<BR><BR>INSTALLED INSERTS AND CURED USING HEAT LAMP WITH BMS 5-107 LOT#AK2KP8383K-1 IAW SRM 53-00-50-2R-0 PAR. 5.S(1) (D-G) AND BAC DWG 144A5810 ID:0127<BR><BR>PROTECTIVE TAPE TO LOWER SURFACE STILL REQUIRES INSTALL.;[04] CORRECTED MEASUREMENTS TABLE WITH UPDATED INFORMATION.;[05] ADDING TO LINE 3; 'THERMOMETER ID: ATS2209 / CAL DUE DATE: 10/2023';[06] CORRECTION TO LINE 3; 'SRM 53-00-50-2R-0 PAR. 5.S(1) (D-G)' SHOULD READ ' SRM 53-00-50-2R-0 PAR. 5.S(1) (D-H)'.;[07] VERIFIED CORRECTIVE ACTION ITEMS 1-6 AND MEASUREMENTS TABLE.;[08] INSTALLED PROTECTIVE TAPE; AND PART MARKED PANEL IAW BOEING DWG 146A5810-127<BR><BR>JOB COMPLETE;[09] VERIFIED CORRECTIVE ACTION ITEM 8. JOB COMPLETE