What was found
FOUND .5 INCH CRACK AT FASTENER HOLE AND TWO RIVETS CRACKED LOWER LEADING EDGE SKIN OF LEFT WING NR 3 SLAT BELOW UPSTOP PAD AREA. ACCOMPLISHED HFEC INSPECTION AND MARKED END OF CRACK IAW 51-00-00 PART 6. STOPPED DRILLED END OF CRACK IAW 51-10-1 PAGE 3. HFEC CONFIRMED CRACK IS CONTAINED IAW 51-00-00 PART 6, FABRICATED DOUBLER IAW 57-50-3 FIG 1. INSTALLED DOUBLER AND FILLER IAW 51-30-5 FIG 1 TREATED, PRIMED AND INSTALLED IAW 57-30-3. (M)