As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND LT WING O/B MID FLAP INBOARD WEB CRACKED AT INBOARD JACKSCREW FAIRING MOUNT BRACKET. THE CRACK WAS .75 LONG. THE CRACKED AREA WAS REMOVED. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, 57-50-1, 51-10-2, 51-30-2, AND MM 51-20-11.