What was found
INTERNAL FUSELAGE SKIN HAD CORROSION UNDER THE BLANKET STANDOFF, FRAMES 14 - 15, STRINGERS 6R - 7R. REPAIRED IAW ES-533/16.984, ISSUE B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL FUSELAGE SKIN HAD CORROSION UNDER THE BLANKET STANDOFF, FRAMES 14 - 15, STRINGERS 6R - 7R. REPAIRED IAW ES-533/16.984, ISSUE B.