Supporting part for connecting e.g. non-heavy element to wall surface of structure of aircraft, has base plate comprising centering portion to be placed in hole to center spacer and self-locking clip, which encloses plate and spacer

摘要

The supporting part (30) has a tubular spacer (36) directed in a first direction approximately perpendicular to a surface of a wall (34) of a structure of an aircraft. A hole is formed at an end of the spacer. A base plate (38) is arranged distinct from the spacer and attached on the surface of the element. The base plate comprises a centering portion to be placed in the hole so as to center the spacer and a self-locking clip (48), which forms a loop in a plane containing the direction and encloses the base plate and the spacer.