Browse Standards AMS4136A
Historical CANCELLED 1996-02-01

Aluminum Alloy, Forgings, 4.3zn 3.3mg 0.6cu 0.2mn 0.2cr, Solution and Precipitation Heat Treated, Low Residual Stresses(Cancelled Feb 1996) AMS4136A

This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of February 1996.
AMS4136
2011-08-10
Latest
Reaffirmed
AMS4136A
1996-02-01
Historical
Canceled

SAE MOBILUS

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

Access SAE MOBILUS »

Add to Cart
Members save up to 12% 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, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn; (2024-T861), Solution Heat Treated and Cold Worked, and Artificially Aged

AMS4271A

View Details

STANDARD

Test Method and Limits for Bow Height of Aluminum Sheet Samples After Chemical Milling

AS6507

View Details

STANDARD

Heat Treatment of Wrought Aluminum Alloy Parts

AMS2770R

View Details

Get Involved

Want to participate in updating this standard?

Join Committee Learn More
X