As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE D-CHECK, A CRACK WAS FOUND ON THE RIGHT WING UPPER LEADING EDGE EXTERNAL PLATING, TWELVE INCHES OUTBOARD OF THE NUMBER THREE PYLON. REPAIR WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING C88-R19 AND ENGINEERING ORDER 57-DC8-510.