Patent ID: 8226033

Claim:
Arrangement for use in an aircraft component installation system, the arrangement comprising: a frame element ( 10 ) which is attachable to an aircraft structure and which comprises two longitudinal struts ( 12 , 14 ) which, at least in sections, are substantially parallel to one another, and which have a curvature that is matched to the curvature of ribs of the aircraft structure, such that the longitudinal struts ( 12 , 14 ), in the mounted state of the arrangement, extend, at least in sections, substantially parallel to the ribs of the aircraft structure, and a storage bin ( 26 ), wherein the frame element ( 10 ) comprises a storage bin fastening device and the storage bin comprises a device which is designed complementary to the storage bin fastening device of the frame element ( 10 ), and wherein the storage bin fastening device of the frame element ( 10 ) and the device of the storage bin ( 26 ) are adapted to rigidly fasten the storage bin ( 26 ) directly slidably to the longitudinal struts at one of a number of various positions along the longitudinal struts ( 12 , 14 ) of the frame element ( 10 ).