Patent ID: 8474758

Claim:
An aircraft component assembly system for use in the assembly of at least one of an interior component, a pipe and an electric line in an aircraft, the aircraft including aircraft structure having a fuselage extending in a longitudinal direction, the aircraft component assembly system comprising: at least one arc-shaped frame element, which comprises a plurality of spaced apart struts that are disposed at least in sections substantially parallel to one another and within a vertical plane transverse to the longitudinal direction, the plurality of struts spanning both side walls and a ceiling of an aircraft cabin structure in a fully assembled state, a connection element that extends between a first and a second end of the frame element and is devised, in the assembled state of the aircraft component assembly system in an aircraft, to form an element of a floor of a cabin of the aircraft, a fastening apparatus for fastening at least one of the interior component, the pipe and the electric line to the frame element or to the connection element, and a first guide device that is provided on the frame element or the connection element and is devised to interact with a second guide device, which is complementary to the first guide device and provided on an aircraft structure, in such a way that the aircraft component assembly system is connectable to the aircraft structure in a manner slideable within the fuselage in the longitudinal direction.