SAE AMS4119E-1990
BARS AND RODS@ ROLLED OR COLD FINISHED 4.4CU - 1.5MG - 0.60MN STRESS-RELIEF STRETCHED (UNS A92024)

Standard No.

SAE AMS4119E-1990

Release Date

1990

Published By

SAE - SAE International

Status

Be replaced 2004-07

Replace By

SAE AMS4119F-1990

Latest

SAE AMS4119F-1990

Scope

Form: This specification covers an aluminum alloy in the form of bars@ rods@ and wire. Application: Primarily for machined parts subject to excessive war page during machining due to residual stress and for parts requiring good strength and whose fabrication does not involve welding. Certain design and processing procedures may cause these products to be susceptible to stress-corrosion cracking; ARP 823 recommends practices to minimize such conditions.

SAE AMS4119E-1990 history

• 1990 SAE AMS4119F-1990 BARS AND RODS@ ROLLED OR COLD FINISHED 4.4CU - 1.5MG - 0.60MN STRESS-RELIEF STRETCHED (UNS A92024)
• 1990 SAE AMS4119E-1990 BARS AND RODS@ ROLLED OR COLD FINISHED 4.4CU - 1.5MG - 0.60MN STRESS-RELIEF STRETCHED (UNS A92024)
• 1979 SAE AMS4119E-1979 ALUMINUM ALLOY BARS, ROLLED, DRAWN, OR COLD FINISHED 4.4Cu - 1.5Mg - 0.60Mn (2024-T351) Stress-Relief Stretched
• 1968 SAE AMS4119D-1968 ALUMINUM ALLOY BARS, ROLLED OR COLD FINISHED 4.4Cu - 1.5Mg - 0.60Mn (2024-T351) Stress-Relief Stretched
• 1966 SAE AMS4119C-1966 ALUMINUM ALLOY BARS, ROLLED OR COLD FINISHED 4.5Cu - 1.5Mg - 0.60Mn (2024-T351) Stress-Relief Stretched
• 1965 SAE AMS4119B-1965 ALUMINUM ALLOY BARS, ROLLED OR COLD FINISHED 4.5Cu - 1.5Mg - 0.6Mn (2024-T351) Stress-Relief Stretched
• 1960 SAE AMS4119A-1960 ALUMINUM ALLOY BARS, ROLLED 4.5Cu - 1.5Mg - 0.6Mn (2024-T351) Stress-Relief Stretched
• 1960 SAE AMS4119-1960 ALUMINUM ALLOY BARS@ ROLLED 4.5Cu - 1.5Mg - 0.6Mn (2024-T3510) Stress-Relief Stretched