Browse Standards AMS4311F
Current REVISED 2019-01-04

Aluminum Alloy, Rolled or Forged Rings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7075-T7351, 7075-T7352) Solution Heat Treated, Mechanically Stress Relieved, and Precipitation Heat Treated AMS4311F

This specification covers an aluminum alloy in the form of rolled or forged rings up to 6 inches (152 mm) inclusive, in nominal thickness at the time of heat treatment, and having an OD to wall thickness ratio of 10 or greater (see 8.6).
AMS4311F
2019-01-04
Latest
Revised
AMS4311E
2012-09-27
Historical
Reaffirmed
AMS4311D
2003-08-05
Historical
Revised
AMS4311C
1994-07-01
Historical
Revised
AMS4311B
1988-10-01
Historical
Revised
AMS4311A
1983-01-01
Historical
Revised
AMS4311
1976-07-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 11% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Aluminum Alloy, Die and Hand Forgings 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr (7175-T74) Solution and Precipitation Heat Treated

AMS4149E

View Details

STANDARD

Aluminum Alloy Forgings and Rolled or Forged Rings 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (6061 - T4) Solution Heat Treated and Naturally Aged

AMS4146G

View Details

STANDARD

Aluminum Alloy Die Forgings (7050-T74) Solution Heat Treated and Overaged

AMS4107G

View Details

Get Involved

Want to participate in updating this standard?

X