As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING I/B FLAP MID SECTION CRACK INDICATION (2) AT CUTOUT I/B EXTENSION MECHANISM. REMOVED FASTENERS PER SRM 51-30-2. STOP DRILLED AT END OF CRACK PER SRM 51-10-1. PERFORMED HFEC INSPECTION PER NDT MAN 51-00-00, NO CRACK PAST STOP DRILL. INSTALLED DOUBLER REPAIR PER SRM 51-10-1. TREATED AND PRIMED PER SRM 51-10-2.