INTERIOR COMPONENT CARRIER SYSTEM AND METHOD FOR MOUNTING AN AIRCRAFT INTERIOR COMPONENT CARRIER SYSTEM

An interior component carrier system (10) comprises a first and a second installation rail (12, 14). Each of the first and the second installation rail (12, 14) includes at least one connecting portion (16) being connectable to an associated primary structure component (18) in order to fasten the installation rail (12, 14) to the primary structure component (18), and a carrier portion (20) extending from the connecting portion (16) in a direction along a longitudinal axis (L) of the interior component carrier system (10). The interior component carrier system (10) further comprises a first carrier element (80) having a first end connected to a first carrier rod (82) extending in a direction along the longitudinal axis (L) of the interior component carrier system (10) and a second end which is connectable to a first interior component (94), wherein the first carrier rod (82) is fastened to the carrier portion (20) of the first installation rail (12, 14), and a second carrier element (84) having a first end connected to a second carrier rod (86) extending in a direction along the longitudinal axis (L) of the interior component carrier system (10) and a second end connected to the first carrier element (80), wherein the second carrier rod (86) is fastened to the carrier portion (20) of the second installation rail (12, 14).