What was found
FLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 UNDER SEAT LOW TRAFFIC SECTION 44.<BR>MULTIPLE PULLED STRANDS; DENTS & OTHER DEFECTS EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4.A-D. PANEL REPLACEMENT REQUIRED.;[02] PANEL FABRICATION/REPLACEMENT IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE.<BR>USING BMS4-23 TYII PANEL MATERIAL LOT 1508290-1 FABRICATED PERFORMED NET TRIM & LOCATED FASTENER HOLES PER DWG 144A5810-116;[03] INSTALLED SL5107A3-410 INSERTS USING BMS5-107 ADHESIVE LOT AK2KP838K-1 THEN CURED IAW SRM 53-00-50-2R-0 PARA 5. S. FIGURE 213 PAGE 30 PER DWG 144A5810-I6 REF CAL TOOL THERMOMETER ID ATS1776 CAL DUE 08/2023;[04] PART MARKED PANEL IAW BOEING DWG 144A5810 ID:0016.;[05] UPDATED MEASUREMENTS;[06] CORRECTION TO CORRECTIVE ACTION 2: DRAWING SHOULD BE 144A5810 ID:0016;[07] CORRECTION TO CORRECTIVE ACTION 3: DRAWING SHOULD BE 144A5810 ID:0016;[08] VERIFIED CORRECTIVE ACTIONS 1-7<BR><BR>VERIFIED MEASUREMENTS TABLE;[09] UPLOADED CURE SHEET. JOB COMPLETE;[10] VERIFIED CORRECTIVE ACTION 9