What was found
ULTRASONIC INSPECTION, SHOWS CRACK INDICATION ON LEFT FLAP INBOARD DRIVE LINK ON INBOARD LUG AT POINT J. REPLACED FLAP DRIVE LINK IAW DC-8 MM 27-51-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ULTRASONIC INSPECTION, SHOWS CRACK INDICATION ON LEFT FLAP INBOARD DRIVE LINK ON INBOARD LUG AT POINT J. REPLACED FLAP DRIVE LINK IAW DC-8 MM 27-51-4.