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SAE International - AS595D

Aerospace - Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump

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Organization: SAE International
Publication Date: 26 October 2015
Status: active
description:

This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance and qualification testing of flat cut-off pressure compensated, variable delivery... View More

Document History

AS595D
October 26, 2015
Aerospace - Civil Type Variable Delivery, Pressure Compensated, Hydraulic Pump
This SAE Aerospace Standard (AS) establishes the general requirements for the design, construction, acceptance and qualification testing of flat cut-off pressure compensated, variable delivery...

References

This document references:
AIR1922 - SYSTEM INTEGRATION FACTORS THAT AFFECT HYDRAULIC PUMP LIFE
Published by SAE International on April 1, 1995
This SAE Aerospace Information Report (AIR) is to present to hydraulic system designers the salient factors that affect hydraulic piston pump life and performance. It is noted that this document...
This document references:
ARP1288 - PLACARDING OF AIRCRAFT HYDRAULIC EQUIPMENT TO IDENTIFY REQUIRED FLUID SUITABILITY
Published by SAE International on July 1, 1974
Details of a durable type and semi-permanently attached placard with prescribed text for the permissible fluids are included in the document.
This document references:
ARP4386 - TERMINOLOGY AND DEFINITIONS FOR AEROSPACE FLUID POWER, ACTUATION, AND CONTROL TECHNOLOGIES
Published by SAE International on January 1, 1992
This document comprises the technical terms and nomenclature together with their definitions and abbreviations used in the field of aerospace fluid power, actuation, and control technologies. The...
This document references:
ARP4752 - AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
Published by SAE International on September 1, 1994
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a hydraulic system that is fitted to a commercial transport aircraft.
This document references:
ARP4925 - AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS
Published by SAE International on January 1, 1996
This SAE Aerospace Recommended Practice (ARP) establishes the factors which should be considered in the design and installation of a hydraulic system fitted to a commercial transport rotorcraft.
This document references:
AS1300 - BOSS - RING LOCKED FLUID CONNECTION TYPE STANDARD DIMENSIONS FOR
Published by SAE International on August 1, 1975
A description is not available for this item.
This document references:
AS19692 - PUMPS, HYDRAULIC, VARIABLE FLOW, GENERAL SPECIFICATION FOR
Published by SAE International on May 1, 1998
This specification and a detail pump specification establish the requirements for variable flow hydraulic pumps, for use in aircraft hydraulic systems conforming to and as defined in MIL-H-5440 and...
This document references:
AS33649 - BOSSES, FLUID CONNECTION, INTERNAL STRAIGHT THREAD
Published by SAE International on April 27, 2004
A description is not available for this item.
This document references:
AS4273 - FIRE TESTING OF FLUID HANDLING COMPONENTS FOR AIRCRAFT ENGINES AND AIRCRAFT ENGINE INSTALLATIONS
Published by SAE International on August 1, 1996
This document establishes requirements, test procedures, and acceptance criteria for the fire testing of fluid handling components and materials used in aircraft fluid systems. It is applicable to...
This document references:
AS4941 - Aerospace - General Requirements for Commercial Aircraft Hydraulic Components
Published by SAE International on May 1, 1998
This specification covers the requirements that are common to most components used in commercial aircraft hydraulic systems. This specification shall be used to develop Procurement Specifications for...
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