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About This Item

 

Full Description

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of March 2012 and has been superseded by AMS4031, AMS4599, ASM4600, AMS4601 and AMS4613. The requirements of the latest issues of AMS4031, AMS4599, ASM4600, AMS4601 and AMS4613 shall be fulfulled whenever reference is made to the cancelled AMS4295. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, noting that is has been superseded..

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

These products have been used typically for parts requiring good weldability, but usage is not limited to such application.

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

Document History

  1. SAE AMS4295D


    Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr (2219 - O, F, T31, T351, T37, T81, T851, T87) (Stabilized: Sep 2013)

    • Most Recent
  2. SAE AMS4295C

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    Aluminum Alloy Sheet and Plate, 6.3Cu - 0.30Mn - 0.06Ti - 0.10V - 0.18Zr (2219 - O, F, T31, T351, T37, T81, T851, T87) (Cancelled: Mar 2012)

    • Historical Version
  3. SAE AMS4295B


    Aluminum Alloy Sheet and Plate 6.3Cu 0.30Mn 0.06Ti 0.10V 0.18Zr(2219 - O, F, T31, T351, T37, T81, T851, T87)

    • Historical Version