This SAE Aerospace Recommended Practice (ARP) describes the design conditions under which tests should be conducted to demonstrate satisfactory performance of a flight critical servo-actuator under the maximum allowable particulate contamination in the associated airplane hydraulic system. Additionally, this document also describes the recommended tests and the required acceptance criteria.
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Aerospace Fluid Power – Contamination Sensitivity – Considerations for Establishing Test Procedures for Flight Control Actuators
SAE International , 10/09/2020
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