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 CORROSION DAMAGE TO TENSION HOLES ON RIGHT UPPER WING SPAR. *S/D* THE RIGHT UPPER AUX SPAR TWO TENSION HOLES WERE SLIGHTLY CORRODED. HOLES WERE REAMED FOR CLEAN-UP AS DOCUMENTED. THESE HOLES ARE WITHIN THE BLUEPRINT TOLERANCES OF 0.781/0.801 IAW DWG 5615057 ZONE B-10, FURTHER REWORK WAS COMPLETED IAW DC-8 SRM 51-1-8.