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General Requirements for the Design and Testing of Civil Type Pressure Compensated, Variable Delivery Hydraulic Pumps
- Aerospace Standard
Published November 02, 2022 by SAE International in United States
This SAE Aerospace Standard (AS) provides general design and test requirements for a flat cut-off pressure compensated, variable delivery hydraulic pump for use in a civil aircraft hydraulic system with a rated system pressure up to 5000 psi (34500 kPa).
NOTE: Hydraulic pumps may incorporate features such as a clutch in the input drive, which will not be covered by this standard.
AS595 has been updated to Revision E for the following reasons:
The title and scope have been revised.
It incorporates technical and editorial changes, including removing all the references to JAR airworthiness regulations.
Data Sets - Support Documents
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A6C4 is responsible for the development of standards, processes, and practices related to Fluid Power Sources (Pumps, Motors, Accumulators), and the integration of these components for Commercial and Military air vehicles. The panel provides a forum for government engineers, prime contractors, and suppliers to exchange technical information, regulatory updates, recent technology developments, issues related to system development and in service operation and lessons learned.
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