What was found
CENTER FUSELAGE LT UPPER SKIN PANEL INNER SURFACE HAS CORROSION, FRAMES 23C-23D, STRINGER 5A-6. REPAIRED PER 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 5A-6. REPAIRED PER SRAS CETS-3143/16.