What was found
AFW FUSELAGE SKIN AT SECTION 48 HAS LIGHT CORROSION BETWEEN STRINGER 30 AND 32 LT AND BETWEEN STATION 1809 AND 1832. AREA OF DISCREPANCY IS 4.8 INCHES BY 20 INCHES. REPAIRED PER MRB 767 3283.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFW FUSELAGE SKIN AT SECTION 48 HAS LIGHT CORROSION BETWEEN STRINGER 30 AND 32 LT AND BETWEEN STATION 1809 AND 1832. AREA OF DISCREPANCY IS 4.8 INCHES BY 20 INCHES. REPAIRED PER MRB 767 3283.