What was found
REMOVED CORROSION DAMAGE BY BLENDING TO A 20 TO 1 RATION. PERFORMED 10X VISUAL AND HFEC INSPECTON TO VERIFY CRACK AND CORROSION FREE. FABRICATED A TAPERED SHIM FROM 2024-T3. FLAT PEENED SURFACE. APPLIED ALODINE AND TWO COATS OF BMS 10-11, TYPE I PRIMER TO BLENDOUT LOCATION. WET INSTALLED 1/32 OVERSIZED HI-LOCKS PROTRUDING HEADS WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW ECO 2948. AIRCRAFT RETURNED TO SERVICE. (M)