As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP LEADING EDGE INTERNAL FORWARD FITTING CRACKED AT STATION XW92.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, AND DC8 SRM 51-1-8B.