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SAE International - ARP4378A

Aerospace - Accumulator, Hydraulic, Welded Bellows, Factory Precharged

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Organization: SAE International
Publication Date: 1 June 2009
Status: active
description:

This Aerospace Recommended Practice (ARP) provides design and test requirements for factory precharged, welded bellows hydraulic accumulators.

Document History

ARP4378A
June 1, 2009
Aerospace - Accumulator, Hydraulic, Welded Bellows, Factory Precharged
This Aerospace Recommended Practice (ARP) provides design and test requirements for factory precharged, welded bellows hydraulic accumulators.

References

This document references:
ARP1383 - IMPULSE TESTING OF HYDRAULIC ACTUATORS, VALVES, PRESSURE CONTAINERS AND SIMILAR FLUID SYSTEM COMPONENTS
Published by SAE International on March 1, 1978
This Aerospace Recommended Practice (ARP) establishes the requirements and the procedures for impulse testing of actuators, valves and pressure containers for use in aerospace hydraulic systems. It...
This document references:
ARP4379 - Accumulator, Hydraulic, Cylindrical Aircraft
Published by SAE International on June 11, 1991
A description is not available for this item.
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:
ARP4553 - Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing
Published by SAE International on July 16, 2002
A description is not available for this item.
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:
AS4059 - AEROSPACE-CLEANLINESS CLASSIFICATION FOR HYDRAULIC FLUIDS
Published by SAE International on June 14, 1988
This SAE Aerospace Standard defines cleanliness levels for particulate contamination of hydraulic fluids and includes methods of reporting data relating to the contamination levels. The contamination...
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...
This document references:
AS5440 - Hydraulic Systems, Aircraft, Design and Installation Requirements For
Published by SAE International on April 1, 1998
This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems.
This document references:
AS8775 - Hydraulic System Components, Aircraft and Missiles, General Specification For
Published by SAE International on November 17, 2008
This specification covers the general requirements that are common to most hydraulic components (see 6.2 ), used in aeronautical hydraulic systems (see 6.1 ).
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