What was found
WHILE UNDERGOING 2 YEAR CHECK INSPECTION, CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL SURFACE BETWEEN FRAMES 24 AND 25, AND STRINGERS 19 RIGHT AND STRINGER 20 RIGHT. SKIN REPAIRED IAW CETS-2231/16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE UNDERGOING 2 YEAR CHECK INSPECTION, CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL SURFACE BETWEEN FRAMES 24 AND 25, AND STRINGERS 19 RIGHT AND STRINGER 20 RIGHT. SKIN REPAIRED IAW CETS-2231/16.