What was found
PASS. CABIN FLOOR PANEL HAS PULLED FIBERS UPPER SURFACE DAMAGE IS ON PANEL 231GF<[01] IDENTIFIED 231GF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 3; TABLE 3.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR><BR>WILL BE PERFORMING WORK IAW SRM 53-00-50-2R-0<BR><BR>FABRICATED NEW PANEL USING BMS 4-17 TY6 LOT: 1514505-1 IAW SRM 53-00-50-2R-0 PARA 1.A.NOTE ALONG WITH DWG 143A5810 SHEET 575<BR><BR>INSTALLED 34EA INSERTS USING BMS 5-107 LOT: AK2KP8383K<BR>CURE RESIN USING THERMOMETER ATS2208 DUE: 10/2023 IAW SRM 53-00-50-2R-0 PARA 5.S.(1) ALONG WITH DWG 143A5810 SHEET 575;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-0.;[03] CORRECTION FOR LINE 1 MEASUREMENT TABLE; CHANGED 'LENGTH AND WIDTH' TO REFLECT DAMAGED PANEL SIZE.<BR><BR>VERIFIED PROTECTIVE TAPE WAS APPLIED TO LOWER SURFACE IAW DRAWING 1433A5810 SHEET 575 'E' CODE E6659.<BR><BR>VERIFIED NEW FABRICATED PANEL WAS PARTMARKED IAW DRAWING 143A5810 SHEET 575 'E' CODES E8818 AND E8102.<BR><BR>JOB COMPLETE.;[04] VERIFIED CORRECTIVE ACTIONS 1-3<BR><BR>VERIFIED MEASUREMENTS TABLE<BR><BR>VALIDATED APPLICABILITY OF SRM 53-00-50-2R-0