What was found
CENTER FUSELAGE FWD KEEL SKIN PANEL HAD CORROSION ON INTERIOR SURFACE AFT OF FRAME 23A BETWEEN STRINGERS 21L - 21R. REPAIRED IAW CETS-5009/16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CENTER FUSELAGE FWD KEEL SKIN PANEL HAD CORROSION ON INTERIOR SURFACE AFT OF FRAME 23A BETWEEN STRINGERS 21L - 21R. REPAIRED IAW CETS-5009/16.