Patent ID: 8770520

Claim:
A device for mounting at least one connector in an aircraft fuselage comprising: a first and second traverse configured to connect the device to a structural section of the aircraft fuselage at end sections of the first and second traverses; a frame element extending traversely between the first and second traverses and configured to accommodate the at least one connector; a first and a second connecting profile respectively connecting the frame element to the first and second traverse; wherein the frame element and the first and second connecting profiles each have a perforation pattern configured to accommodate at least one attachment, and wherein the first and second traverses each include a C-shaped profile with a web, a first flange and a second flange, the web, the first flange and the second flange each having a perforation pattern extending along the entire length of the traverses such that the frame element is flexibly moveable in a longitudinal and vertical direction with respect to each of the traverses.