What was found
TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 FILLERS AND REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN, MIN .5 INCH OUTSIDE CORNER RADIUS WITH 2.0 INCH INSIDE CORNER RADIUS AND 5D-6D SPACING AT NEW FASTENER LOCATIONS. FINISH ALL BARE ALUMINUM WITH ALODINE AND TWO COATS OF BMS 10-11 TYPE 1, PRIMER. INSTALLED FILLERS AND REPAIR DOUBLER WITH FASTENERS INDICATED IN FIGURES 1, 2, AND TABLE 1. APPLIED FILLET SEAL OF BMS'S 5-95 SEALANT AROUND EDGES OF REPAIR, BS 420, 440, 460, 480 AND 767. VERIFIED 8110-3 RECEIVED. REPAIR COMPLETED IAW ECO3250, DEVIATION AF. AIRCRAFT RETURNED TO SERVICE. (M)