What was found
(AUS) FUSELAGE TOP SKIN CORRODED BETWEEN SKIN AND DOUBLER ANGLES AT LAP JOINT. PART TC: 6,471.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(AUS) FUSELAGE TOP SKIN CORRODED BETWEEN SKIN AND DOUBLER ANGLES AT LAP JOINT. PART TC: 6,471.