SAE MA4510
Current
The latest, up-to-date edition.
Fittings, Weld, Fluid Connection, 35 000 kPa, Metric
Hardcopy , PDF
English
21-08-2015
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1 SCOPE
2 REFERENCES
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
This SAE Metric Aerospace Standard (AS)Establishes the requirements for weld fluid connection fittings and rings to be orbital arc welded to tubing for use in metric aircraft fluid systems at a maximum operating pressure of 35,000 kPa.
| DocumentType |
Standard
|
| Pages |
16
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
This SAE Metric Aerospace Standard (AS) establishes the requirements for weld fluid connection fittings and rings to be orbital arc welded to tubing for use in metric aircraft fluid systems at a maximum operating pressure of 35,000 kPa.
| SAE AIR5426 | Fitting and Fitting Assembly Selection, Installation, Inspection and Maintenance of |
| SAE MA 4510/1 : 1996 | FITTINGS, WELD TO 24 DEGREE CONE FLARELESS, FLUID CONNECTION, METRIC |
| 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 |
| SAE MA2023A | ALTERNATE DIMENSIONS, CENTER BODY SECTION, SHAPE FLUID FITTING, DESIGN STANDARD, METRIC |
| MIL H 46170 : B | HYDRAULIC FLUID, RUST INHIBITED, FIRE-RESISTANT, SYNTHETIC HYDROCARBON BASE |
| SAE AMS5656F | Steel, Corrosion Resistant, Bars, Wire, Forgings, Extrusions, and Rings 9.0Mn - 20Cr - 6.5Ni - 0.27N Solution Heat Treated |
| 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) |
| SAE MA 4510/1 : 1996 | FITTINGS, WELD TO 24 DEGREE CONE FLARELESS, FLUID CONNECTION, METRIC |
| 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 AMS4945F | Titanium Alloy Tubing, Seamless, Hydraulic 3Al - 2.5V, Controlled Contractile Strain Ratio Cold Worked, Stress Relieved |
| SAE MA2094 | Test Methods for Tube-Fitting Assemblies, Metric (ISO 10583) |
| SAE AS1241D | Fire Resistant Phosphate Ester Hydraulic Fluid for Aircraft |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| SAE MA2307A | FITTING END, INTEGRAL CENTERED WELD LIP, DESIGN STANDARD, METRIC |
| 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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