SAE AMS2801A

Heat Treatment of Titanium Alloy Parts.

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Standard:
  • AMS2801
  • Revision: A
Revised:
  • 1994-09-01
Revision:
  • Historical. Access the latest revision: AMS2801B
Issuing:
  • Ams Amec Aerospace Metals And Engineering Committee
Scope:

This specification covers the engineering requirements for heat treatment by part fabricators (users) or their vendors or subcontractors of parts made from the following titanium alloys: Commercially pure; 3AL-2.5V; 5Al-2.5Sn; 8Al-1Mo-1V; 6Al-4V; 6Al-4V(ELI); 6Al-6V-2Sn; 6Al-2Sn-4Zr-2Mo; 6Al-2Sn-4Zr-6Mo; 3Al-8V-6Cr-4Mo-4Zr; 13V-11Cr-3Al; 10V-2Fe-3Al; 15V-3Cr-3Al-3Sn.

History:
StandardPublishedRevisionStatus
AMS2801B2003-03-12LatestReaffirmed
AMS2801A1994-09-01HistoricalRevised
AMS28011990-07-01HistoricalIssued
AKA:
  • SAE AMS 2801
Sector:
  • Aerospace
Topic:
  • Metallurgy
  • Metals
  • Nonferrous alloys
  • Materials properties

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