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, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE LOWER RIB OUTBOARD ACCESS PANEL 518. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION A REPAIR ANGLE IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL 57-2-0 AND ENGINEERING ORDER 57-DC8-1764.