What was found
623AT INBD STRESS PANEL FLANGE PITTED AND FRETTED ALONG INBD FLANGE. LOCALLY BLEND PITTING AND FRETTED AREA ON LADDER PLATE. COMPLIED WITH HIGH FREQUENCY EDDY CURRENT INSP CRACK CHECK, NO DEFECTS NOTED. REPAIRED IAW EO8-57-10-0611.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
623AT INBD STRESS PANEL FLANGE PITTED AND FRETTED ALONG INBD FLANGE. LOCALLY BLEND PITTING AND FRETTED AREA ON LADDER PLATE. COMPLIED WITH HIGH FREQUENCY EDDY CURRENT INSP CRACK CHECK, NO DEFECTS NOTED. REPAIRED IAW EO8-57-10-0611.