SAE AS 603 : 2015
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
06-30-2015
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.
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.
| Committee |
G-3
|
| DevelopmentNote |
Supersedes SAE ARP 603. (07/2008) Supersedes SAE MA 2002. (11/2013)
|
| DocumentType |
Revision
|
| Pages |
6
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| 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 AS1576E | FITTINGS, WELDED, HYDRAULIC, TITANIUM, CORROSION RESISTANT STEEL AND NICKEL, 3000 PSI HYDRAULIC |
| SAE AS4459B | 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 ARP994B | 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 AS1975G | 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 | 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.