As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 3 INCH CRACK AT SPLICE PLATE ON LOWER SURFACE OF LT WING UPPER LEADING EDGE SKIN DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR, FSS 224. THE SPLICE PLATE WAS CUT OUT, A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-2.