As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING NR 5 LEADING EDGE SLAT CLOSER PANEL HAS A CRACK. ACP INTERIM RPR PER SRM AND ECRA USING 2024-T3 .040 ALUM, PICKING UP EXISTING BOLTS AND 4 RIVETS DOUBLER. MUST DO A VISUAL INSP EVERY A-CHECK AND ACCOMPLISH A PERMANENT REPAIR WITHIN 100 DAYS.