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  • SAE AS 603 : 2015

    Current The latest, up-to-date edition.

    IMPULSE TESTING OF HYDRAULIC HOSE, TUBING, AND FITTING ASSEMBLIES

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  30-06-2015

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1 SCOPE
    2 REFERENCES
    3 REQUIREMENTS
    4 METHOD OF TEST
    5 INTENDED USE
    6 NOTES
    7 NOTES

    Abstract - (Show below) - (Hide below)

    This SAE Aerospace Standard (AS) establishes the requirements and procedures for impulse testing of hose, tubing, and fitting assemblies for use in aerospace hydraulic systems of 8000 psi nominal operating pressure or less.

    General Product Information - (Show below) - (Hide below)

    Committee G-3
    Development Note Supersedes SAE ARP 603. (07/2008) Supersedes SAE MA 2002. (11/2013)
    Document Type Revision
    Publisher SAE International
    Status Current
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE AS 6116 : 2016 ALUMINUM FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPERABLE, FLUID SYSTEM, UP TO 1500 PSI (10340 KPA) MAXIMUM, SPECIFICATION FOR
    MIL-DTL-8790 Revision F:2007 Hose Assemblies, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +275 Degrees F, Field Attachable
    MIL-DTL-32330 Revision A:2015 Hose Assembly, Conductive Polytetrafluoroethylene Tube, Smooth Bore, Flared and Flareless, Tube to Hose, with Swivel Nut
    MIL-DTL-8788 Revision G:2015 Hose, Rubber, Hydraulic, High Pressure 3,000 PSI, Operating Temperature Range -65 Degrees F to +160 Degrees F
    SAE AS 1576 : 2016 FITTINGS, WELDED, HYDRAULIC, TITANIUM, CORROSION RESISTANT STEEL AND NICKEL, 3000 PSI HYDRAULIC
    SAE AS 4459 : 2013 FITTINGS, TUBE, FLUID SYSTEM 3000 PSIG (21000 KPA) RATED PRESSURE, EXTERNALLY SWAGED, SPECIFICATION FOR
    MIL-DTL-25427 Revision B:2009 COUPLING ASSEMBLY, HYDRAULIC, SELF SEALING, QUICK DISCONNECT, GENERAL SPECIFICATION FOR
    MIL-DTL-83296 Revision B:2009 Fittings, Corrosion Resistant Steel, High Temperature, High Pressure (3000 PSI), Hydraulic and Pneumatic, General Specification for
    MIL-DTL-83298 Revision C:2009 Hose, Conductive Polytetrafluoroethylene Tube, High Temperature, High Pressure (3000 PSI), Hydraulicand Pneumatic
    SAE AS 85720 : 2018 FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE BEAM SEAL, 5000/8000 PSI, GENERAL SPECIFICATION FOR
    SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
    SAE AS 5958 : 2017 FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR
    SAE AS 1975 : 2016 Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
    SAE AS 4157 : 2017 COUPLING ASSEMBLIES, HYDRAULIC, SELF-SEALING, QUICK DISCONNECT, 8000 POUNDS PER SQUARE INCH, GAGE
    SAE AS 5960 : 2013 HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, METALLIC BRAID REINFORCED, 5080 PSI (35000 KPA), 400 DEGREES F (204 DEGREES C), AIRCRAFT HYDRAULIC SYSTEMS
    MIL-DTL-8794 Revision F:2007 HOSE, SYNTHETIC RUBBER - HYDRAULIC FLUID, FUEL, AND OIL RESISTANT
    10/30203850 DC : 0 BS ISO 6772 - AEROSPACE - FLUID SYSTEMS - IMPULSE TESTING OF HYDRAULIC HOSE, TUBING AND FITTING ASSEMBLIES
    SAE AS 2078 : 2015 TEST METHODS, HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE (PTFE)
    SAE ARP 1383 : 2013 AEROSPACE - IMPULSE TESTING OF HYDRAULIC COMPONENTS
    MIL-DTL-5070 Revision F:2006 ADAPTER, HOSE TO TUBE, PIPE AND FLANGE, REUSABLE - HYDRAULIC, FUEL, AND OIL LINES, GENERAL SPECIFICATION FOR
    MIL-DTL-8789 Revision G:2015 FITTING END, ATTACHABLE, HYDRAULIC, HIGH PRESSURE (3,000 PSI), GENERAL SPECIFICATION FOR
    SAE AS 5000 : 2010 FITTING, PLUG-IN UNION, RING LOCKED, 24 DEGREE CONE, FLUID CONNECTION, 5080 PSI (35000 KPA), SPECIFICATION FOR
    SAE AS 5620 : 2017 TITANIUM HYDRAULIC TUBING, TI-3AL-2.5V COLD WORKED AND STRESS RELIEVED, UP TO 35000 KPA (5080 PSI), REQUIREMENTS FOR QUALIFICATION TESTING AND CONTROL
    SAE ARP994C:2023 Design of Tubing Installations for Aerospace Hydraulic Systems

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL-PRF-7808 Revision L:1997 LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE
    ISO 6772:2012 Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies
    SAE AIR 1228 : 2009 STANDARD IMPULSE MACHINE EQUIPMENT AND OPERATION
    MIL-PRF-83282 Revision D:1997 HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537
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