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ALUMINUM RIVETS, UNS A92117 2.5Cu - 0.3Mg (2117-T4)
- Aerospace Standard
- AS7222
- Issued
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers rivets fabricated from an aluminum alloy designated as 2117-T4, solution treated.
Topic
Data Sets - Support Documents
No Datasets Available
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
| Number | Title |
|---|---|
| AMS2355 | TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings |
| AMS2470 | PROTECTIVE TREATMENTS for ALUMINUM BASE ALLOYS |
| AMS2770 | HEAT TREATMENT OF ALUMINUM AND ALUMINUM-BASE ALLOYS |
| ANSI/Y14.5M | This document is not part of the subscrption. |
| AS125251THRUAS1 | This document is not part of the subscrption. |
| AS125701THRUAS1 | This document is not part of the subscrption. |
| ASTMB565 | This document is not part of the subscrption. |
| MIL-STD-105 | This document is not part of the subscrption. |
| MIL-STD-1312 | This document is not part of the subscrption. |
| MIL-STD-2073-1 | This document is not part of the subscrption. |
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