As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT PIT SKIN CORRODED AT FS 1356 TO FS 1359 STRINGER 39L TO STRINGER 38L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH B767-200 SRM 53-00-01. ORIGINAL MATERIAL THICKNESS IS .105 MATERIAL REMAINING .057 MATERIAL REMOVED .048. FABRICATED AND INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH B767-200 SRM 53-00-01. UT GAUGE TOOL T8225I.