As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ALC STA 1065 LOWER INTERNAL SKIN AND STRINGERS BETWEEN FUSELAGE DRAINS HAVE SURFACE CORROSION. BLEND OUT REQUIRED AT CORRODED AREA, REMOVED CORRODED AREA AT LOWER FUSELAGE SKIN STA 1080 TO STA 1131, STRINGER 38L TO 38R IAW B767-200 SRM 53-60-01 ALLOWABLE DAMAGE 2.DID UT INSP FOUND TO OUT OF LIMITS INSTALLED DOUBLER AND TRIPLER IAW REA47401REA14 REV A