As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON INTERNAL FUSELAGE SKIN STA 783 ABOVE STRINGER 13R. REMOVED CORROSION FROM INTERNAL FUSELAGE SKIN AT STA 783 ABOVE STR 12R, IAW B767 200 SRM 53-00-01 AD 1. WITH 0.027" MAT LOSS, DAMAGE EXCEEDED 15% ALLOWED & FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW REA NO 47416REA10.