Hello. Sign In
Standards Store




SAE AMS4366

2014 Edition, December 1, 2014

Complete Document

Aluminum Alloy, Extruded Profiles (2065-T84) 4.2Cu - 1.2Li – 0.52Mg – 0.32Mn – 0.32Ag - 0.1Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged



Detail Summary

Active, Most Current

EN
Format
Details
Price (USD)
PDF
Single User
$78.00
Print
In Stock
$78.00
Add to Cart

Product Details:

  • Revision: 2014 Edition, December 1, 2014
  • Published Date: December 2014
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 5
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:

Form

This specification covers an aluminum-lithium alloy in the form of extruded profiles with a maximum cross-sectional area of 19 square inches (123 cm2) and a maximum circle size of 11 inches (279mm) from 0.040 to 0.499 inches (1.00 to 12.50 mm) in thickness (See 8.5).

Application

These extrusions have been used typically for machined parts requiring high strength and good corrosion resistance, but usage is not limited to such applications. 

Certain processing procedures may cause this product to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such condit
AIA/NAS Aerospace Standards