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 13L RUNNING NEXT TO TEAR STRAP. REMOVED CORROSION FROM INTERNAL FUSELAGE SKIN AT STA 783 ABOVE STR 12L, IAW B767-200 SRM 53-00-01 AD1. WITH 0.002" MAT LOSS, DAMAGE FOUND TO BE BEYOND 15% ALLOWED AND BEYOND LIMITS. REPAIRED DAMAGE IAW REA NO 47416REA49.