As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A MAINTENANCE VISIT, FOUND LT WING FLAP FITTING (P/N 5652807) HAS ELONGATED HOLE AT HINGE END AT XW 4.0. REMOVED BASE FITTING IAW DC-8 SRM 51-3-2. REAMED HOLE TO 0.6735 IAW SRM 51-3-2 AND FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03724. FABRICATED AND INSTALLED NEW BUSHING IAW REO-03724 AND DAC DWG 5652691.