As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON FLAP EXTENSION FOR LANDING, SPLIT FLAPS WERE INDICATED. CONFIRMED BY ROLL TENDENCY. LEFT FLAP WAS APPROXIMATELY 6 DEGREES BEHIND RIGHT FLAP. RIGHT FLAP AT 35 DEGREES, LEFT FLAP AT 29 DEGREES. FOUND LEFT INBOARD FLAP ACTUATOR IDLER ARM TRACK MISSING NUT AND HANGING. REPLACED MISSING NUT. INSPECTED FLAPS. RAN FLAPS UP AND DOWN SEVERAL TIMES. NO SPLIT NOTED IAW DC-8 MM 27-51-03.