What was found
RT WING TOP AFT PANEL PLATING CRACKED 4" STA XCW 69.500 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20, SHEET 1. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED AREA + FABRICATED (-5) DOUBLER (7075"0" 0.160") + (-7) TRIPLER (7075"0" 0.125") + FILLER (7075T651 PLATE 0.312") IAW SRM 57-2-1 FIG. 20 SHEET 1, SRM 57-3-3 FIG. 13 ITEM "L", SRM 51-10-0 FIG. 1 SHEET 23. NDT INSPECTED CUT OUT AREA. NO CRACK FOUND IAW NDT SPM PART 08-00-002 TO 07. NO CRACK FOUND. ENCLOSED SMN FORM 242-4. HEAT TREATED REPAIR PARTS IAW SRM 51-1-1 PG 1-13-17, DPS 7.001. ENCLOSED (4EA) FORMS SMN 075. CLEANED AND APPLIED POLYURETHANE TOP COATING TO AREA IAW SRM 51-1-12 PG 7. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG 20 SHEET 1, SRM 51-1-11 (PRC) SRM 51-1-26 (CONICAL SPACER: RIVETS TYPE MS20426DD) SRM 51-1-20D, SRM 51-3-1 (TORQUE) (TORQUE WRENCH: SNAP ON, MODE: QC1R200, SN: 0896200457) (INSP CRITERIA: VISUAL METHOD, INITIAL REPETITIVE INSP NORMAL MX, REPLACEMENT: N/A IAW SRM 57-0-1 PG 4, TR57-105, DATED 12-23-09)