1650-00-226-2514
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A mechanical fluid passage joint designed for linkage of aircraft rigid hydraulic lines and components subject to pivotal, linear, or rotational position changes. The device allows two-directional flow of high pressure fluid and permits single plane rotation upon its axis. It may also allow for angular movement. Excludes:swivel joint, pipe; and swivel joint, tube.
1650-00-226-2514, no name available
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