What was found
LT WING INBOARD L/E SLANT PANEL UPPER CAP CORRODED STA XFS 138.750 - 151.250. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-3-0 PG 1. PERFORMED BLENDEOUT (7.125*1.875*0.092) FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. PERFORMED VISUAL DETAIL INSPECTION, NO CORROSION NOR CRACK FOUND. FABRICATED FILLER (AL7075T6 0.080) AND EXTERNAL REPAIR DOUBLER (AL7075T6 0.125) IAW BOEING SKETCH 05-04-18-001, SRM 57-2-1 FIG 37. CLEANED, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-1-8B. INSTALLED FILLER ON SLANT PANEL UPPER CAP WITH PRC SEALANT IAW SRM 51-1-15 PG 1, BOEING SKETCH 03-04-18-001, SRM 57-2-1 FIG 31 AND EXTERNAL REPAIR DOUBLER. TORQUED IAW SRM 51-3-1.