Standard

SAE ARP5941

Oct 2020 Published

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Language English

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Abstract

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.

Document information

Standard from SAE International
Published: 9 October 2020
Document type: IS
Pages
ISBN:

Publisher SAE International
Distributor SAE International

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Referred by: SAE ARP5796

SAE ARP5941

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