Patent ID: 8888053

Claim:
An aircraft conduit harness retention system comprising: a first part having an attachment formation for attachment to an aircraft component at a first end and a first mating formation at a second end; a second part having a second mating formation; and a conduit harness separate from the second part, wherein said conduit harness includes a wire loom receiving portion and a flange connected to the wire loom receiving formation, the flange having a bore defined therethrough, wherein the bore of the flange is engaged by one of the first mating formation and second mating formation and the first mating formation and the second mating formation are engaged via a snap-fit to secure the flange of the conduit harness between the first and second parts such that the conduit harness is offset from the aircraft component, wherein the the second part has a third mating formation defined at an end opposite the second mating formation, the third formation engageable with a further second mating formation of a further mount cap to retain a flange of a conduit harness therebetween.