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SAE AS7222A

Superseded

Superseded

View Superseded by

Aluminum Rivets, UNS A92117 2.5Cu - 0.3Mg (2117-T4) Procurement Specification

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

11-21-2018

Superseded date

09-28-2019

Superseded by

SAE AS7222B

US$112.10
Excluding Tax where applicable

1 SCOPE
2 REFERENCES
3 TECHNICAL REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 ACKNOWLEDGEMENT
7 REJECTIONS
8 NOTES

Covers rivets made from an aluminum alloy designated as 2117-T4, solution treated.

DevelopmentNote
Supersedes SAE AMS 7222 (07/1999)
DocumentType
Standard
Pages
9
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

This procurement specification covers rivets made from an aluminum alloy designated as 2117-T4, solution treated. The following specification designations and their rivet coatings are covered:

SAE AMS2770M Heat Treatment of Wrought Aluminum Alloy Parts
MIL-STD-2073-1 Revision E:2008 Standard Practice for Military Packaging
SAE AMS2355L Quality Assurance, Sampling and Testing Aluminum Alloys and Magnesium Alloy Wrought Products (Except Forging Stock), and Rolled, Forged, or Flash Welded Rings
MIL-STD-105 Revision E:1989 Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information)
SAE AMS2470N Anodic Treatment of Aluminum Alloys Chromic Acid Process

US$112.10
Excluding Tax where applicable