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SAE AS603B

Current

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

$141.19
Including GST where applicable

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

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.

DevelopmentNote
Supersedes SAE ARP 603. (07/2008) Supersedes SAE MA 2002. (11/2013)
DocumentType
Standard
Pages
6
PublisherName
SAE International
Status
Current
Supersedes

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. It also refers to standard impulse test equipment to be used in conducting these impulse tests.

SAE AS6116A Aluminum Fittings, Axially Swaged Tube with Flareless Separable, 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 AS1576E Fittings, Welded, Hydraulic, Titanium, Corrosion Resistant Steel and Nickel, 3000 psi Hydraulic
SAE AS4459B Fittings, Tube, Fluid System 3000 psig (21 000 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 AS85720B Fittings, Tube, Fluid Systems, Separable, High Pressure Beam Seal, 5000/8000 psi, General Specification For
SAE ARP994B Design of Tubing Installations for Aerospace Hydraulic Systems
SAE AS5958F Fittings, Axially Swaged Tube with Flareless Separable, Fluid System for Operating Pressures up to and Including 5080 psi (35000 kPa), Specification for
SAE AS1975G Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
SAE AS4157B Coupling Assemblies, Hydraulic, Self-Sealing, Quick Disconnect 8000 Pounds Per Square Inch, Gage
SAE AS5960B Hose Assembly, Polytetrafluoroethylene, Metallic Braid Reinforced, 5080 psi (35 000 kPa), 400 °F (204 °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 AS2078A 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 AS5000C Fitting, Plug-in Union, Ring Locked, 24 Degree Cone, Fluid Connection, 5080 psi (35 000 kPa), Specification for
SAE AS5620B 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 Design of Tubing Installations for Aerospace Hydraulic Systems

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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