Patent attributes
A device for securing aircraft wiring includes a first body having a first end, a second end opposite the first end, and a concave portion extending semi-annularly between the first end and the second end, the concave portion having a surface defining a wire-receiving space. In an embodiment, the device includes a grip connection element configured to slidably mate with a gripping element. In an embodiment, the device includes a first hole extending into the second end, a first recess extending from the first hole, and a first tab including a first portion and a first latch, the first portion of the first tab projecting in a first direction from the first end of the first body, the first latch of the first tab projecting in a second direction from the first portion of the first tab, the first hole configured to receive a tab identical to the first tab.
