schematic representation a tool 6 which defines a contour of the construction component 1 to be adhered though illustrated as straight here the tool can also be curved or have some other shape for example the tool 6 can be molded from worn out damage in a component of an aircraft the construction component 1 to be adhered is applied onto the tool 6 e g in the form of a laminate with the planar formation 2 e g in the form of a release sheet as well as the passages 3 thus transferring the contour thereof the curable liquid 4 is poured into and solidified in the passages 3 the construction component 1 to be adhered having the planar formation 2 and the cured liquid 4 is removed from the tool 6 the planar formation 2 is pulled away and the construction component 1 having the spacers 5 formed in this way from the cured liquid 4 see fig4 are adhered in place of the worn out damage in the aircraft component preferably the planar formation 2 having the curable or already cured liquid 4 may remain on the first construction component 1 until immediately before the adhesion to the second construction component or until immediately before a surface treatment thus acting as a protective film for example fig4 shows in a schematic representation the construction component 1 to be adhered with spacers 5 here the spacers 5 have the form of knobs are circular in shape and are distributed uniformly in rows across the construction component the knobs can ensure a predetermined bond gap thickness or minimum bond gap thickness additionally it should also be noted that.