SAE AMS4472
SAE AMS4472 Aluminum Alloy, Plate 4.0Cu - 1.0Li - 0.40Mg - 0.35Ag - 0.13Zr (2195-T34) Solution Heat Treated and Stress Relieved
standard by SAE International, 06/06/2011
Full Description
This specification covers an aluminum alloy in the form of plate.This plate has been used typically for aerospace structural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications. Material is delivered in T34 temper and precipitation heat treated to obtain T82 temper by the end user.Cart
(empty)
New products
- IEC 62908-12-10 Ed. 2.0 en:2023
- IEC 62471-7 Ed. 1.0 b:2023
- IEC 62087-3 Ed. 2.0 b:2023
- IEC 61970-SER Ed. 1.0 b:2023
- IEC 60332-SER Ed. 1.0 b:2023
- IEC 61158-5-4 Ed. 4.0 b:2023
- IEC 61784-1-3 Ed. 1.0 b:2023
- IEC 61784-1-0 Ed. 1.0 b:2023
- IEC 62769-150-1 Ed. 2.0 b:2023
- IEC 61784-2-21 Ed. 1.0 b:2023
- IEC 63171-7 Ed. 1.0 en:2023
- IEC 63474 Ed. 1.0 b:2023
- IEC 60534-1 Ed. 4.0 b:2023
- IEC 62106-6 Ed. 2.0 en:2023
- IEC 60071-2 Ed. 5.0 b:2023
- IEC 60601-2-46 Ed. 4.0 b:2023
- IEC 61156-11 Ed. 2.0 en:2023
- IEC 61189-2-801 Ed. 1.0 b:2023
- IEC 61189-2-803 Ed. 1.0 b:2023
- IEC 61340-2-3 Ed. 2.0 b Cor.1:2023
Specials
-
-
BS EN 50673:2019
$160.02 (-58%) $67.21