What was found
TRIMMED OUT DAMAGED WEB. HFEC INSPECTED THE EDGE OF CUTOUT. ENLARGED TRIM BY .04 AS A INSURANCE CUT. FABRICATED A .50 INCH THICK REPAIR WEB, TOW .063 INCH THICK DOUBLERS AND A .063 INCH THICK TAPER FILLER FROM 2024-T3 CLAD SHEET. FABRICATED THREE EACH REPAIR STIFFENERS FROM7075-T6511 EXTRUSION. FABRICATED A 50:1 TAPER FILLER FROM 2024-T3 CLAD. FLAT PEENED REPAIR T-STIFFENERS. ALODINED AND PRIMED REPAIR PARTS AND BARE ALUMINUM. INSTALLED REPAIR PARTS IAW FIGURE 3, USING FASTENERS IDENTIFIED, WET WITH BMS 5-95 SEALANT MAINTAINING 5D TO 6D SPACING AT NEW LOCATIONS. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M)