As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 2 INCH CRACK AT SPLICE PLATE INSIDE LEFT WING UPPER LEADING EDGE ABOVE NR 2 LEADING EDGE FLAP ACTUATOR/ANTI-ICE DUCT AREA, WS 224.5. THE SPLICE PLATE WAS REMOVED AND A STRAP WAS FABRICATED AND INSTALLED IAW SRM 57-50-2 AND 51-30-2.