What was found
TRIMMED AREA AND VERIFIED CRACK REMOVED USING HFEC. FABRICATED 3 EACH FILLERS AND A REPAIR DOUBLER FROM 2024-T3 AS SHOWN IN PHOTO 1, MAINTAINING 2D EDGE MARGIN 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 DOUBLERS WITH FASTENERS INDICATED IN FIGURES 1, 2 AND TABLE 2. APPLIED FILLET SEAL OF BMS 5-95 SEALANT AROUND EDGES OF REPAIR. REPAIR COMPLETED IAW ECO 3250, DEVIATION AG. WINDOW FRAME P/N 65-465271, 291, 311, 321 AND 65-465491, BS 420, 440, 460, 480 AND 767. AIRCRAFT RETURNED TO SERVICE. (M)