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Assembling of Studs in Aluminum and Magnesium
- Aerospace Standard
- ARP142C
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This document covers the recommended basics to be considered when assembling cadmium plated steel studs with rolled threads into cast, or forged, aluminum or magnesium parts.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature. This standard has been stabilized.
Recommended Content
| Aerospace Material Specification | Protective Treatments Magnesium Alloys |
| Aerospace Material Specification | Pressure Testing, 25 Psi |
| Aerospace Material Specification | Pressure Testing, 70 Psi |
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE 2 |
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
Reference
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