As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, LBL 102. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 99. ORIGINAL MATERIAL THICKNESS = 0.220 INCH, REMAINING MATERIAL THICKNESS = 0.185 INCH, MATERIAL REMOVED = 0.035 INCH AND FOUND ACCEPTABLE AS PER EA 8-5730-159860. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 115.