As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SKIN CORRODED BS 1241 JUST BELOW STRINGER 34R. CORROSION ON SKIN WAS FOUND TO BE OUT LIMITS. SKIN THICKNESS OF .210, REMAINING THICKNESS .100 IN ACCORDANCE WITH B767 SRM 51-00-01 TABLE I DETAIL II. REPAIRED PER AMES ENGINEERING DOCUMENT 47224REA44 REV A.