A COMPONENT ARRANGEMENT ON AN AIRCRAFT STRUCTURE, AND A METHOD FOR THE INSTALLATION OF A COMPONENT INTO AN AIRCRAFT STRUCTURE

摘要

Disclosed is a component arrangement on an aircraft structure (2), in particular on a fuselage structure of an aircraft (4), with at least one mounting structure (6) connected with the aircraft structure (2), and at least one component (10) to be assigned to the aircraft structure (2), in particular a measuring device. In accordance with the invention at least one component carrier (8) is provided for the reception of the component (10) to be mounted, wherein the component carrier (8) can be connected with the mounting structure (6), and an outer surface (24) of the component carrier (8), facing away from the component (10), extends approximately flush with an outer surface of the aircraft structure (2). Also disclosed is a method for the Installation of a component (10) into an aircraft structure (2) with a mounting structure (6), wherein the component (10) is connected with the mounting structure (6) via a component carrier (8), and an outer surface (24) of the component carrier (8), facing away from the component (10), extends approximately flush with an outer surface of the aircraft structure (2).