SAE AMS4163G

Действует

Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

Описание Изменения Ссылки Версии

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Standard Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum Alloy Products — 6 стр.

SAE AMS4163F

Заменен

Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

На этот документ ссылаются

SAE AMS4163D

Заменен

Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

SAE AMS4163E

Заменен

Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

SAE AMS4163F

Заменен

Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

SAE AMS4163A

Заменен

ALUMINUM ALLOY EXTRUSIONS 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated and Stress-Relieved by Stretching

SAE AMS4163B

Заменен

ALUMINUM ALLOY EXTRUSIONS 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated and Stress-Relieved by Stretching

SAE AMS4163C

Заменен

Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

SAE AMS4163

Заменен

ALUMINUM ALLOY EXTRUSIONS 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Stress-Relief Stretched and Straightened