As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING LEADING EDGE NUMBER 2 SLAT HAS CRACK ACROSS FASTENER IN COVE AREA FORWARD OF INBOARD MAIN DRIVE TRACK ARM MARKED. STOP-DRILLED CRACK PER AARD 57-43-00-4. ACCOMPLISHED HIGH FREQUENCY EDDY CURRENT AROUND STOP DRILL. NO CRACK INDICATION BEYOND STOP DRILL. INSTALLED DOUBLER PER AARD 57-43-00-4.