As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON CENTER WING AUX TANK TOP PANEL SURFACE AT BS 1199-1219, X = -75 TO X = -107. CORROSION REMOVED AS PER MD-11 SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.247 INCH; MATERIAL REMOVED = 0.014 INCH; MATERIAL REMAINED = 0.233 INCH - FOUND EXCEEDED LIMIT AS PER SRM 57-10-01 REV 47, FIGURE 101. ACCOMPLISHED E.A. 1-5710-149871, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 113.