A device for connecting two construction components (10, 12) that are have engagement structures (16) on two connection surfaces (14) that are facing each other, in which the components (10, 12) have at least two pairs of oppositely disposed circular arc-shaped engagement structures (16) each of which extends over an angle of not more than 180 and has at least one open end, the engagement structures being arranged such that the center of the circular arc of the engagement structure of one pair is different from the center of the circular arc of the engagement structure of each other pair, and at least two connectors (22) are provided, each of which has engagement structures (24) complementary to the engagement structures (16) of one pair and adapted to be inserted in a rotary movement into the two engagement structures (16) from the open end.

A bolt assembly for connecting component sections of an aircraft component is disclosed and includes a guard that is assembled onto threads of a bolt. The guard includes a first end, a second end and an outer surface having a uniform diameter between the first end and the second end. The bolt assembly further includes a nut including internal threads securable to the external threads of the bolt.

A force-applying element for fixing radomes provides an annular flange region. The force-applying element provides at least one fixing region, which extends from the flange region in the direction towards the radome to be fixed, and its outer surfaces are surrounded by the radome in a form-fit manner.