As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING NUMBER 7 SLAT LEADING EDGE HAS SKIN CORROSION, ADJACENT TO A FASTENER LOCATION ON THE LEADING EDGE SKIN SURFACE APPROX 2.5 FEET INBOARD OF THE OUTBOARD EDGE. CORROSION BLENDED TO FINAL SKIN THICKNESS OF .023 INCH. CUT OUT DAMAGE PER AARD. FABRICATED AND INSTALLED REPAIR DOUBLERS PER AARD 57-43-01.