What was found
FORWARD FUSELAGE II SKIN CORROSION AT FRAME 13, STRINGER 18R - 21R. PERFORMED REPAIR IAW AEA ERS-EM-53MR-123.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD FUSELAGE II SKIN CORROSION AT FRAME 13, STRINGER 18R - 21R. PERFORMED REPAIR IAW AEA ERS-EM-53MR-123.