What was found
CUTOUT THE DAMAGED FROM THE VERTICAL LEG. BLENDED OUT REMAINING AREA OF THE CHORD MAINTAINING A GREATER THAN .050 INCH THICKNESS. PERFORMED 10X VISUAL AND HFEC INSPECTION TO VERIFY CRACK AND CORROSION FREE. FLAP PEENED REWORKED SURFACES. FABRICATED REPAIR PARTS 1, 2, 3 AND 4 FROM 2024-0 PER FIGURE 1. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II PRIMER TO ALL BARE SURFACES. INSTALLED REPAIR PARTS WITH FASTENERS IDENTIFIED. REPAIR COMPLETED IAW ECO 2948 R4. AIRCRAFT RETURNED TO SERVICE. (M)