Hydraulic Systems & Equipment encompasses the design, integration and certification of complete aircraft hydraulic circuits operating typically at 3,000–5,000 psi, covering system architecture, pressure regulation, flow control valves, manifolds and associated line-replaceable units (LRUs) compliant with AS603, MIL-H-5440 and related airworthiness standards, including redundant multi-circuit configurations for flight-control and landing-gear actuation duties.
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