What was found
AFT FLOOR PANEL 242WF UPPER AND LOWER SKINS HAVE PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 6; <BR>TABLE 6; AND BOEING DWG DOC: 147A5810 ID: 0010.<BR><BR>PANEL DAMAGE TO UPPER SKIN PLIES IS OUT OF ALLOWABLE DAMAGE LIMITS IAW <BR>SRM 53-00-50-1A-1 PAR. 4. F.<BR><BR>PANEL DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-1 FOLLOWING SRM <BR>53-00-50-2R-0 PAR. 2. A. TABLE 201<BR><BR>REMOVED ALL INSERTS AND SANDED AWAY DAMAGED PLIES ON UPPER FACESHEET <BR>AND LOWER FACESHEET CLEANED IAW SRM 53-00-50-2R-1 PAR. 3. A. - F. OK <BR>TO POT OPEN CORE.[06] CURED POTTING; SANDED FLUSH; CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES FROM BMS9-3 STYLE 1581 LOT 1522395-2 IAW SRM 53-00-50-2R-1 PARAGRAPH 3.H-J AND K.(1).(A). OK TO INSTALL REPAIR PLIES.[09] INSTALLED REPAIR PLIES TO TOOLSIDE AND BAGSIDE USING BMS8-201 TY 4 EPOCAST 50-A <BR>(946) LOT# 1527294-1; SET UP VACUUM BAG SYSTEM WITH BLEED DOWN TEST CHECKED <BR>GOOD AND NO LEAKS USING GAUGE ID: ATS2441 CAL/DUE: 08/2023 IAW SRM <BR>53-00-50-2R-1 PAR. 3. K. (1) (B) (C) & 3. L. (1) (A) - (C). OK TO CURE.