As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON CTR WING TANK TOP PANEL SURFACE AT STA 1210 , X = -8 TO X = 8. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL MATERIAL THICKNESS = 0.172 INCH; MATERIAL REMOVED = 0.008 INCH; MATERIAL REMAINED = 0.112 INCH - FOUND EXCEEDED LIMIT AS PER MD-11 SRM 57-10-01 REV 47, FIGURE 101. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 113.