Frame element, aircraft component assembly system and method of fitting a component in an aircraft

摘要

A frame element (10; 10′) for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at least one insulation pack (52) to the frame element (10; 10′). An aircraft component assembly system (46) comprises a plurality of such frame elements (10; 10′). In a method of fitting a component (34, 52) in an aircraft, a frame element (10; 10′) is provided. At least one interior component (34) or at least one insulation pack (52) is fastened to the frame element (10; 10′). Then the frame element (10; 10′) having the at least one interior component (34) or the at least one insulation pack (52) fastened thereto is attached to an aircraft structure (36).