What was found
TRIMMED OUT CRACK, VERIFIED CRACK FREE USING HFEC INSPECTION. ENLARGED TRIM BY .040 INCH INSURANCE CUT. HFEC INSPECTED ALL FASTENER HOLES. FABRICATED A .071 INCH STRUCTURAL FILLER, .063 INCH INNER PLATE, .063 INCH PLATE, .125 OUTER PLATE AND .0180 INCH THICK FILLER FROM 2024-T3 CLAD SHEET AS SHOWN IN FIGURE 1. ALODINED AND TWO COATS BMS 10-79, TYPE III PRIMER TO REPAIR PARTS AND EXPOSED SURFACES. INSTALLED REPAIR PARTS. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES OF THE REPAIR. REPAIR COMPLETED IAW ECO 3396. AIRCRAFT RETURNED TO SERVICE. (M)