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SAE International - ARP4553

Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing

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Organization: SAE International
Publication Date: 16 July 2002
Status: active

Document History

ARP4553
July 16, 2002
Accumulator, Hydraulic, Cylindrical Aircraft, Self-Displacing
A description is not available for this item.

References

This document references:
AIR4543 - AEROSPACE HYDRAULICS AND ACTUATION LESSONS LEARNED
Published by SAE International on January 13, 1992
This Aerospace Information Report (AIR) contains technical information on aerospace hydraulic and actuation technologies lessons learned. The lessons learned were prepared by system designers and...
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:
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:
ARP4150 - PROCEDURE FOR INSPECTION OF INSERVICE AIRBORNE ACCUMULATORS FOR CORROSION AND DAMAGE
Published by SAE International on March 18, 2011
This SAE Aerospace Recommended Practice (ARP) is intended as a guide in establishing inspection procedures to determine the condition of inservice accumulators. A minimum inspection program is...
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:
ARP598 - PROCEDURE FOR THE DETERMINATION OF PARTICULATE CONTAMINATION OF HYDRAULIC FLUIDS BY THE PARTICLE COUNT METHOD
Published by SAE International on November 1, 1991
This test describes a self-checking procedure for the determination of particulate contaminant five microns or greater in size in hydraulic fluids by the particle count method. A maximum variation of...
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:
AS4716 - AEROSPACE STANDARD, GLAND DESIGN, O-RING AND OTHER ELASTOMERIC SEALS
Published by SAE International on June 11, 1993
This SAE Aerospace Standard provides standardized gland (groove) design criteria and dimensions for elastomeric seal glands for static and dynamic applications. The glands have been specifically...
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:
MA2012 - PORT CONNECTION INTERNAL, STRAIGHT THREAD, METRIC
Published by SAE International on September 1, 1982
A description is not available for this item.
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