As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
COROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT STA 1219 TO STA 1239, X = -27.5 TO X = -47.5. CORROSION REMOVED AS PER MD-11 SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.041INCH; MATERIAL REMAINED = 0.131 INCH - FOUND EXCEEDED LIMIT AS PER MD-11 SRM 57-10-01 REV 47, FIGURE 101. ACCOMPLISHED EA 1-5710-149871. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 113.