What was found
PASSENGER CABIN FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DUE TO THE EXTENT OF DAMAGE CUT NEW FLOOR PANEL FROM BMS 4-23TY2 LOT#1479169-1 IAW SRM 53-00-50-2R-0 PARA 1A(NOTE) AND BOEING DWG 144A5810-127.;[02] VALIDATED APPLICABILITY OF SRM 53-00-50-2R-0.;[03] INSTALLED THROUGH INSERTS USING BMS5-107 CLASS 1 LOT#AK0DP4051K. SET TO CURE USING HEAT LAMP AND THERMOMETER ID:ATS2208 S/N:43300740WS. COMPLETED SUCCESSFUL CURE; AND INSTALLED SEALANT TAPE BMS8-283TY1 LOT#0CN050418. IAW BOEING DWG 144A5810-127; AND BAC5085 FIGURE 15 PAR.8.4.2.2 (A-H);[04] ADDITION TO LINE 3: ADDED PART MARK TO PANEL 241AF;[05] VALIDATED LINE 4;[06] ADDITION TO LINE 4: ADDING PART MARK REFERENCE IAW BOEING DWG 144A5810-127; AND BOEING DWG 140A1008;[07] VERIFIED CORRECTIVE ACTIONS 1-6