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 CRACK ON THE LT WING L/E INTERNALLY 28 1/2 INCHES FWD OF WING SPAR UPPER CORD AT XILD .7095, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW DC-8 SRM 51-1-21 AND DAC DWG 3269743.