What was found
INTERNAL FUSELAGE SKIN HAS LEVEL 2 CORROSION AT FRAMES 33 - 34, STRINGERS 12 - 13R. REPAIRED IAW SRAS ES-121/18.12361.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE SKIN HAS LEVEL 2 CORROSION AT FRAMES 33 - 34, STRINGERS 12 - 13R. REPAIRED IAW SRAS ES-121/18.12361.