As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C LT WING I/B MAIN FLAP DRIVE ARM UPPER FITTING LWR FLANGE CRACKED, CRACK AT BOTH I/B & O/B FLANGE. LT WING I/B MAIN FLAP DRIVE ARM UPPER FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44, THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AND 10134-2007-7075 T6 AS REPAIR ANGLES REPAIR SIZE 2 X 4 INCHES.