What was found
RIGHT WING COMPOSITE FIXED LEADING EDGE UPPER SURFACE IS DELAMINATED FROM OFSS 655 TO OFSS 683.<[01] IDENTIFIED R/H O/B UPPER FIXED LEADING EDGE MATERIAL ACCORDING TO SRM 57-41-01-0I-3; FIG. 4; TABLE 4; ITEM 1; AND FIG. 8; TABLE 8. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1; PARA'S 2.B AND 4.B.(5); AND FIG. 101. <BR><BR>AREAS TO BE REPAIRED ACCORDING TO SRM 51-70-05-2R-4; AS REQUIRED BY SRM 57-41-01-2R-1; PARA'S 2.F; 4.B.(1); AND TABLE 201.<BR><BR>STRIPPED UPPER SURFACE PAINTS/PRIMERS; REMOVED LOWER SURFACE BONDED ALUMINUM FOIL; REMOVED DELAMINATED PLIES AND CORE TO A REGULAR SHAPE THRU BOTH BOTH FACESHEETS; APPROX. 51' FROM O/B END; AND 8' FROM THE FWD EDGE; TAP TESTED AREAS (NO DISBONDS NOTED); REMOVED CONTAMINANTS FROM REPAIR AREA; ALL ACCORDING TO SRM 51-70-05-2R-4; PARA'S 4.A AND 4.B.; AND SRM 51-70-14-2R-3. PARA. 4.A.(2).(B).;[12] FABRICATED ALUMINUM FOIL REPAIR PLY FROM BMS 8-289 LOT#1507307-1; INSTALLED WITH BMS 5-128 LOT#JH2FAL7046; VACUUM BAGGED; LEAK CHECK GOOD; CURED; UNBAGGED AND TRIMMED EXCESS MATERIAL IAW SRM 51-70-14-2R-3 PARA 4(3-5)(11)(A-L) AND BOEING DWG 116A5411 FL11.<BR>APPLIED ALUMINUM TAPE 3M Y425 LOT#1514681-1 ACROSS FWD EDGE IAW BOEING DWG 116A5411 FL 11.<BR>REFINISHED OUTER SURFACE IAW SRM 51-70-05-2R-4 PARA 4.M.<BR><BR>THERMOMETER ID:ATS2208 CAL DUE 10/2023<BR>VACUUM GAUGE ID:ATS2441 CAL DUE 08/2023<BR>MULTIMETER ID:ATS1658 CAL DUE 03/2023;[13] VERIFIED CORRECTIVE ACTION #12