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Fittings, Weld, Fluid Connection, 5000 psi Maximum
- Aerospace Standard
- AS4510A
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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 up to a maximum operating pressure of 5000 psi.
Rationale
Qualification specifics for weld-to-beam seal reduced-wall/reduced-pressure fittings are not included in AS85421, AS85720, AS4510, or AS4510/2. This revision will clarify qualification requirements for those fitting versions. Additionally, dash codifications that are on current detail standards, but not in AS4510, are being added.
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| Table 1 | Materials | |
| Table 2 | Tubing wall thickness, operating pressure, and flexure test stress for weld fittings with type 21-6-9 corrosion resistant steel tubing | |
| Table 3 | Tubing wall thickness, operating pressure, and flexure test stress for weld fittings with type 3.0AI 2.5V titanium alloy tubing | |
| Table 4 | Test samples for performance tests | |
| Table 5 | Quality conformance inspection | |
| Unnamed Dataset 9 | ||
| Table A1 | Classes of defects, defect characteristics, and AQLs | |
| Table A2 | Fitting end design, weld | |
| Table A3 | Ring, weld | |
| Table A4 | Straight fitting (adapter, reducer) weld to separable fitting | |
| Table A5 | Shape fitting (tee, elbow, cross) weld and weld to separable fitting |
Issuing Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
This Committee is responsible for developing and maintaining standards for design, test, and procurement of fluid systems part standards to improve reliability and economy. Their primary focus is on AS standards development and support of military standards. The Committee also develops ISO standards in a Subcommittee Advisory Group (SCAG) to ISO/TC 20/SC 10, and SAE-MA derivatives thereof.
Structure: SAE G-3 -- Parent committee SAE G-3A -- Aerospace Couplings Subcommittee SAE G-3B -- Aerospace Fittings Subcommittee SAE G-3D -- Aerospace Hose Subcommittee SAE G-3E - Aerospace Tubing Assemblies Subcommittee U.S. SCAG to ISO/TC 20/SC 10 -- ISO standards Major projects: Support of Military Standards Reform Support of military standard conversions to MIL-PERF and MIL-DTL. Development of AS replacements for military standards designated for conversion. Establish document to list G-3 accepted replacements for replaced part standards and military back-up specifications. Development of PRI QML/QPL Development of Performance Review Institute (PRI) process for approval and surveillance of manufacturers (Qualified Manufacturer List, QML) and for approval of standard parts as qualified for use (Qualified Parts List, QPL). Development of ISO Standards, Imperial Units ISO/TC 20/SC 10 standards have typically been developed in SI units. The ISO has approved development of inch-based ISO standards to support commercial aviation. Basic design, test, and procurement specifications will be selected from military standards that are to be converted to Non-Government standard (NGS) and developed as ISO standards.Reference
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