SAE AMS4298 PDF

SAE AMS4298 PDF

Name:
SAE AMS4298 PDF

Published Date:
07/22/2004

Status:
Active

Description:

Aluminum Alloy, Alclad Sheet, 3.8Cu - 1.0Mg - 0.3Mn - 0.60Zn (Alclad 2056-T3) Solution Heat Treated and Cold Worked

Publisher:
SAE International

Document status:
Active

Format:
Electronic (PDF)

Delivery time:
10 minutes

Delivery time (for Czech version):
200 business days

SKU:
sae-ams4298_1172478

Choose Document Language:
18.30 €
Need Help?
This specification covers an aluminum alloy in the form of sheet clad on both sides.

These products have been used typically for formed structural aircraft parts requiring improved resistance to fatigue crack growth and high toughness with strength similar to Alclad 2024-T3, but usage is not limited to such applications.
File Size : 1 file , 330 KB
Note : This product is unavailable in Ukraine, Russia, Belarus
Published : 07/22/2004

History

SAE AMS4298B
Published Date: 03/12/2024
Aluminum Alloy, Alclad Sheet 3.8Cu - 1.0Mg - 0.30Mn - 0.60Zn (Alclad 2056-T3) Solution Heat Treated and Cold Worked (Stabilized: Mar 2024)
22.20 €
SAE AMS4298
Published Date: 07/22/2004
Aluminum Alloy, Alclad Sheet, 3.8Cu - 1.0Mg - 0.3Mn - 0.60Zn (Alclad 2056-T3) Solution Heat Treated and Cold Worked
18.30 €

Related products

SAE AMS6493B
Published Date: 11/05/2018
Steel Bars, Forgings, and Tubing 1.0Cr - 3.25Ni - 0.40Mo (0.17 - 0.22C) Electroslag Remelted or Consumable Electrode Vacuum Remelted Premium Aircraft-Quality
22.20 €
SAE AMS4021H
Published Date: 05/30/2017
Aluminum Alloy, Alclad Sheet and Plate, 1.0Mg - 0.60Si - 0.28Cu - 0.20Cr (Alclad 6061-0) Annealed (Stabilized: May 2017)
23.70 €

Best-Selling Products