What was found
CORROSION ON THE FUSELAGE INTERIOR SKIN FROM STRINGER 33 TO 35R. BS 1085. REPAIRED IAW ENGINEERING DOCUMENT 4722REA41.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON THE FUSELAGE INTERIOR SKIN FROM STRINGER 33 TO 35R. BS 1085. REPAIRED IAW ENGINEERING DOCUMENT 4722REA41.