What was found
POSSIBLE CORROSION BETWEEN SKIN AND STRINGER 18L CAUSING RIVET HEAD TO CRACK, DUE TO EXPANSION OF CORROSION. PERFORMED PERMANENT REPAIR OF FUSELAGE SKIN AT FR 61 AND STGR 18L IAW EO1-53-21-0204.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
POSSIBLE CORROSION BETWEEN SKIN AND STRINGER 18L CAUSING RIVET HEAD TO CRACK, DUE TO EXPANSION OF CORROSION. PERFORMED PERMANENT REPAIR OF FUSELAGE SKIN AT FR 61 AND STGR 18L IAW EO1-53-21-0204.