As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND BETWEEN FS 1375 AND 1417 STR 35R AND 36R. BLENDED CORROSION BETWEEN STA 1375 TO 1417 STR 35R TO 36R. ORIGINAL THICKNESS .074", REMOVED .041", REMAINING T .033" FOUND TO BE OUT OF LIMITS. REQUESTED ENGINEERING SUPPORT. RECEIVED AMES DOC 47416REA13 FOR REPAIR. OUT OF LIMITS, IAW B767 200 SRM 53-00-01. REPAIRED IAW AMES DOC 47416REA13.