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Revision C, November 1, 2004

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Aluminum Alloy, Alclad Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti Alclad 2219-T31; Sheet, Solution Heat Treated and Cold Worked Alclad 2219-T351; Plate, Solution Heat Treated and Stress Relieved

Includes all amendments and changes through Reaffirmation Notice , April 2012

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Product Details:

  • Revision: Revision C, November 1, 2004
  • Published Date: April 2012
  • Status: Active, Most Current
  • Document Language: English
  • Published By: SAE International (SAE)
  • Page Count: 7
  • ANSI Approved: No
  • DoD Adopted: No

Description / Abstract:


This specification covers an aluminum alloy in the form of alclad sheet and plate.


These products have been used typically for parts requiring high strength up to 600 °F (316 °C) and are also well suited for cryogenic applications and where welding and maximum corrosion-resistance are required, but usage is not limited to such applications.

Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking after heat treatment; ARP823 recommends practices to minimize such conditions.

AIA/NAS Aerospace Standards