What was found
CENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23C-23D, STRINGER 6A-7. REPAIRED IAW SRAS 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 23C-23D, STRINGER 6A-7. REPAIRED IAW SRAS CETS-3143/16..