| CPC F16L 27/023 (2013.01) [B64D 37/005 (2013.01); F16L 3/16 (2013.01); B64D 37/30 (2013.01); F16L 9/18 (2013.01)] | 16 Claims |

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1. An aircraft pipework assembly comprising: an aircraft structure; pipework; a fixture arrangement between the pipework and the aircraft structure; a tie rod; a first tie rod bearing which connects the tie rod to the pipework; and a second tie rod bearing which connects the tie rod to the aircraft structure; wherein the fixture arrangement comprises a spherical bearing, the spherical bearing comprising a ball mounted to the pipework and a housing coupled to the aircraft structure; the ball comprises a convex spherical bearing surface; the housing comprises a concave spherical bearing surface which mates with the convex spherical bearing surface of the ball; and the fixture arrangement is configured to enable the pipework to translate relative to the ball in an axial direction aligned with a longitudinal axis of the pipework.
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