SAE AMS4162

Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T8511) Solution Treated, Stress Relief Stretched, Straightened, and Precipitation Heat Treated.

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Standard:
  • AMS4162
Revised:
  • 1968-05-01
Revision:
  • Historical. Access the latest revision: AMS4162D
Issuing:
  • Ams D Nonferrous Alloys Committee
Scope:

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing.

These extrusions have been used typically for structural parts requiring high strength up to 500 degrees F (260 degrees C), but usage is not limited to such applications. May be welded in the specified condition but properties are improved by reheat treatment after welding. Reheat treatment after welding, however, may reduce resistance to stress-corrosion cracking.

History:
StandardPublishedRevisionStatus
AMS4162D2003-07-28LatestReaffirmed
AMS4162C1998-03-01HistoricalRevised
AMS4162B1990-04-01HistoricalRevised
AMS4162A1977-01-01HistoricalRevised
AMS41621968-05-01HistoricalIssued
AKA:
  • SAE AMS 4162
Sector:
  • Aerospace
Topic:
  • Aluminum alloys
  • Aluminum

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