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 A 5 INCH CRACK TO THE LWR SURFACE OF THE RT WING LEADING EDGE SKIN APPROX. 16 INCHES FWD OF THE WING FRONT SPAR AT XRS 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW 51-1-21, 51-1-20D.