SAE AMS4330A

Aluminum Alloy, Plate (2297-T87) 2.8cu 1.5li 0.30mn 0.25mg Solution Heat Treated, Stretched, and Artificially Aged.

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Standard:
  • AMS4330
  • Revision: A
Revised:
  • 2003-07-14
Revision:
  • Historical. Access the latest revision: AMS4330B
Issuing:
  • Ams D Nonferrous Alloys Committee
Scope:

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

These products have been typically used in aerospace applications where low density is needed in combination with moderate strength, high fatigue resistance, good stress corrosion properties, and improved stiffness, but usage is not limited to such applications.

History:
StandardPublishedRevisionStatus
AMS4330B2004-11-24LatestReaffirmed
AMS4330A2003-07-14HistoricalRevised
AMS43302001-11-19HistoricalIssued
AKA:
  • SAE AMS 4330
Sector:
  • Aerospace
Topic:
  • Aluminum alloys

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