As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#5 LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIBS HAS WORKING FASTENERS / REMOVED WORKING FASTENERS IAW SRM 51-40-02-0G-0 AT #5 L/E SLAT NOSE SKIN AT ACTUATOR. FOUND CRACK ON O/B FASTENER HOLE. REMOVED AND REPAIRED L/E SLAT SKIN DAMAGE IAW SRM 57-42-01-2R-8