What was found
INTERNAL FUSELAGE SKIN CORRODED BETWEEN FRAME 13 - 14, STRINGER 18R - 20R. PERFORMED REPAIR IAW AEA ERS-EM-53MR-210.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE SKIN CORRODED BETWEEN FRAME 13 - 14, STRINGER 18R - 20R. PERFORMED REPAIR IAW AEA ERS-EM-53MR-210.