As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING REPETITIVE COMPLIANCE WITH A/D 2001-06-02 & S/B 57-90 R5 DETECTED 2 EACH CRACK INDICATIONS IN NON ADJACENT ATTACHMENT HOLES OF THE FORWARD LEG OF THE RIGHT WING FRONT SPAR LOWER CAP. REPAIRED 2 EACH CRACKED HOLES IAW DC-8 S/B 57-90 R5 TABLE 4, CONDITION NR 2 AND STRESS COINED REMAINING HOLES TO CONDITION NR 1,OPTION 2.