As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION DETECTED DURING NDT IN AFT INBOARD BOLT HOLE OF FLAP FWD HINGE SUPPORT FITTING AT WS 128.00 LH WING. CRACK LOCATED .150" FROM SKIN SURFACE, .090" LENGTH, 040" DEEP. COMPLETED REPAIR IN AFT INBD BOLT HOLE OF FLAP FWD HINGE SUPPORT FITTING AT WS 128.00 L/H WING IAW REO 670-57-21-907.