SAE AS 1896 : 2013

Superseded

View Superseded by

COUPLING ASSEMBLY, SELF-SEALING, ONE SIDE ONLY, HYDRAULIC

Available format(s)

Hardcopy , PDF

Superseded date

14-01-2019

Language(s)

English

Published date

01-01-2013

Publisher

SAE International

1 SCOPE
2 REFERENCES
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES

Establishes the requirements for aircraft, hydraulic couplings, self sealing one side only, for use in Type 2 hydraulic systems (-65 to +275 degree F temperature range) as defined by MIL-H-5440.

Committee	G-3
DocumentType	Standard
Pages	17
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE AS 1896B:2019
Supersedes	SAE AS 1896 : 1991

SAE ARP 4752 : 2013	AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
SAE ARP 4925 : 2014	AEROSPACE DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT HELICOPTER HYDRAULIC SYSTEMS

SAE ARP 24 : 2013	DETERMINATION OF HYDRAULIC PRESSURE DROP
SAE ARP 603 : 1985	IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES
MIL-STD-129 Revision R:2014	Military Marking for Shipment and Storage
MIL-STD-130 Revision N:2007	IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
SAE ARP 868 : 2013	METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS
MIL-STD-810 Revision G:2008	ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL H 25579 : E	HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
SAE AIR 1047 : 2000	A GUIDE FOR THE SELECTION OF QUICK-DISCONNECT COUPLINGS FOR AEROSPACE FLUID SYSTEMS
SAE ARP 908 : 2013	TORQUE REQUIREMENTS, INSTALLATION AND QUALIFICATION TEST, HOSE AND TUBE FITTING
MS33656 Revision J:1987	FITTING END, STANDARD DIMENSIONS FOR FLARED TUBE CONNECTION AND GASKET SEAL
MIL-F-85720 Base Document:1985	FITTING, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM, SEAL, GENERAL SPECIFICATION FOR
MIL-R-8791 Revision D:1982	RETAINER, PACKING, HYDRAULIC, AND PNEUMATIC, TETRAFLUOROETHYLENE RESIN
MIL H 83282 : C	HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537
MIL-H-8775 Revision D:1976	HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
MIL-H-5440 Revision H:1993	HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR
MIL H 5606 : G	HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE
MIL-P-83461 Revision B:1980	PACKING, PREFORMED, PETROLEUM HYDRAULIC FLUID RESISTANT, IMPROVED PERFORMANCE AT 275 DEGREES F (135 DEGREES C)
SAE AS 604 : 2012	HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC REINFORCED, 3000 PSI, 400 DEGREES F, HEAVYWEIGHT, HYDRAULIC
MS33514 Revision G:1990	FITTING END, STANDARD DIMENSIONS FOR FLARELESS TUBE CONNECTION AND GASKET SEAL (ASG)
MIL H 85800 : 0	HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID FIBER REINFORCED, 5000 & 8000 PSI, GENERAL SPECIFICATION FOR
MIL-F-85421 Revision B:1986	FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, BEAM SEAM, 3000/4000 PSI - GENERAL SPECIFICATION FOR

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SAE AS 1896 : 2013

Superseded

Table of Contents

Abstract

General Product Information

Standards Referenced By This Book

Standards Referencing This Book

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