As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NUMBER 7 SLAT HAD CORROSION AT LEADING EDGE SKIN SURFACE APPROXIMATELY 24 INCHES IN FROM OUTBOARD END AT FASTENER. CUT AWAY CORROSION AND CRACK DAMAGE AT APPROXIMATELY 24 INCHES FROM OUTBOARD END AND INSTALLED A FLUSH REPAIR PER SRM 57-43-01-2R.