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Aluminum Rivets, UNS A91100, 99Al (1100-H14)
- Aerospace Standard
- AS7220
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers rivets fabricated from an aluminum alloy designated as 1100-H14, strain hardened.
Rationale
This document has been reaffirmed to comply with the SAE 5-year Review policy.
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Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
TABLE 1 | Composition, Percentages by Weight | |
TABLE 2 | Rivet Head Circular Runout Tolerance |
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 |
ANSI/Y14.5M | 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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