What was found
LEFT FLAP INBOARD HINGE, INTERNAL HINGE ATTACH FITTING WAS CRACKED ON THE OUTBOARD AFT CORNER. REMOVED AND REPLACED FLAP IAW DC-9 MM 27-51-01-4-0201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FLAP INBOARD HINGE, INTERNAL HINGE ATTACH FITTING WAS CRACKED ON THE OUTBOARD AFT CORNER. REMOVED AND REPLACED FLAP IAW DC-9 MM 27-51-01-4-0201.