Connecting assembly for connecting two aircraft structures, aircraft part comprising such assembly, and aircraft

A connecting assembly for connecting two structures of an aircraft, the connecting assembly comprising:

• a central element featuring a through-hole configured to make a connection with a first of said two structures,
• a fastener element inserted into the through-hole,
• a plurality of deformable first shock-absorbing elements, each of the plurality of deformable first shock-absorbing elements being secured to said central element and configured to bear against a surface of a second of said two structures,
• a plurality of second shock-absorbing elements, manufactured from a deformable material, and secured to the central element, each of the plurality of second shock-absorbing elements comprising at least one of a metal insert, an insert made from a material other than said deformable material, or a cavity arranged in the deformable material,
• each deformable first shock-absorbing element extending outwardly from the central element in a direction perpendicular to a longitudinal axis of said through-hole,
• a deformable first shock-absorbing element in the plurality of deformable first shock-absorbing elements comprises a plate extending laterally outwardly, the plate having a plurality of apertures configured to receive fasteners therethrough, and
• each second shock-absorbing element extending outwardly from the central element in a direction perpendicular to the longitudinal axis of said through-hole, which direction is different from a direction in which each first deformable shock-absorbing element extends.