SAE AS4510
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Fittings, Weld, Fluid Connection, 5000 psi
Hardcopy , PDF
29-03-2019
English
07-01-2013
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1 SCOPE
2 REFERENCES
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
APPENDIX A CLASSIFICATION OF DEFECTS
Establishes the requirements for weld fluid connection fittings and rings to be orbital arc welded to tubing for use in aircraft fluid systems at a maximum operating pressure of 5000 psi.
| DocumentType |
Standard
|
| Pages |
19
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
This SAE Aerospace Standard (AS) establishes the requirements for weld fluid connection fittings and rings to be orbital arc welded to tubing for use in aircraft fluid systems at a maximum operating pressure of 5000 psi.
| SAE AS 4510/1 : 1996 | FITTINGS, WELD TO 24 DEGREE CONE FLARELESS, FLUID CONNECTION |
| SAE AIR5426 | Fitting and Fitting Assembly Selection, Installation, Inspection and Maintenance of |
| SAE AS4510/2 | Fittings, Weld To Beam Seal, Fluid Connection |
| SAE AMS5659S | Steel, Corrosion-Resistant, Bars, Wire, Forgings, Rings, and Extrusions 15Cr - 4.5Ni - 0.30Cb (Nb) - 3.5Cu |
| SAE ARP603G | Impulse Testing of Hydraulic Hose, Tubing, and Fittings Assemblies |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL H 46170 : B | HYDRAULIC FLUID, RUST INHIBITED, FIRE-RESISTANT, SYNTHETIC HYDROCARBON BASE |
| SAE AS4510/2 | Fittings, Weld To Beam Seal, Fluid Connection |
| MIL-H-6875 Revision H:1989 | HEAT TREATMENT OF STEEL RAW MATERIALS |
| SAE AMS5561G | Steel, Corrosion and Heat-Resistant, Welded and Drawn or Seamless and Drawn Tubing 9.0Mn - 20Cr - 6.5Ni - 0.28N High-Pressure Hydraulic |
| SAE ARP1185B | Flexure Testing of Hydraulic Tubing Joints and Fittings |
| SAE AMS2759E | Heat Treatment of Steel Parts General Requirements |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| MIL H 83282 : C | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537 |
| MIL H 6083 : E | HYDRAULIC FLUID, PETROLEUM BASE, FOR PRESERVATION AND OPERATION |
| SAE AS1579D | FITTING END, INTEGRAL WELD, LIP, DESIGN STANDARD |
| SAE AMS4945F | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved |
| MIL-STD-12 Revision D:1981 | ABBREVIATIONS FOR USE ON DRAWINGS, SPECIFICATIONS FOR STANDARDS AND IN TECHNICAL DOCUMENTS |
| SAE AS1376D | ALTERNATE DIMENSIONS, CENTER BODY SECTION, SHAPE FLUID FITTING, DESIGN STANDARD |
| SAE AS4697B | FITTING END, INTEGRAL CENTERED WELD LIP, DESIGN STANDARD |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| SAE AMS4944L | Titanium Alloy Tubing, Seamless, Hydraulic 3.0Al - 2.5V Cold Worked, Stress Relieved |
| SAE AS 4510/1 : 1996 | FITTINGS, WELD TO 24 DEGREE CONE FLARELESS, FLUID CONNECTION |
| SAE ARP4784A | Definitions and Limits, Metal Material Defects and Surface and Edge Features, Fluid Couplings, Fittings and Hose Ends |
| SAE AS478N | Identification Marking Methods |
| ISO 10012-1:1992 | Quality assurance requirements for measuring equipment Part 1: Metrological confirmation system for measuring equipment |
| SAE AMS4928V | Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6Al - 4V Annealed |
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