What was found
CENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23B - 23C, STRINGER 7A - 8L. REPAIRED IAW CETS-3143/16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23B - 23C, STRINGER 7A - 8L. REPAIRED IAW CETS-3143/16.