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This paper addresses an experimental study of the pull-out and shear failure loads of composite sandwich insert joints. For specimen fabrication, a Nomex honeycomb core and a carbon–epoxy composite were used. The film-type adhesive FM73 was used for core and face co-cured bonding. Specimen sizes are 120×120mm 2 for the pull-out test and 60×120mm 2 for the shear loading test. About...