As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO CRACKS EMANATING FROM FASTENER HOLES IN THE SKIN OF THE ACTUATOR ATTACHMENT FITTING ON THE LOWER SKIN OF THE LEADING EDGE NR 6 SLAT. ONE CRACK IS .10" AND THE OTHER IS 1.10". ACCOMPLISHED PERMANENT REPAIR OF SLAT IAW SRM 57-42-01-2R.