As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING- LEADING EDGE COMPARTMENT STIFFENER AT XOS 541 FOUND CRACK ABOUT 0.5 INCHES. RIGHT WING LEADING EDGE COMPARTMENT CRACKED STIFFENER AT XOS 541 REMOVED AS PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED STIFFENER AS PER DOUGLAS DRAWING ARB2918 REVISION G, AND INSTALLED FABRICATED STIFFENER PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.