SAE AMS4183A-2011
Aluminum Alloy, Extruded Profiles (2027-T3511) 4.4Cu 1.2Mg 0.8Mn 0.10Zr Solution Heat Treated and Stress Relieved by Stretching

Standard No.

SAE AMS4183A-2011

Release Date

2011

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced

Replace By

SAE AMS4183A-2016

Latest

SAE AMS4183A-2016

Scope

This specification covers an aluminum alloy in the form of extruded profiles.

SAE AMS4183A-2011 Referenced Document

• ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 2024-04-19 Update
• ASTM B645-10 Standard Practice for Linear-Elastic Plane-Strain Fracture Toughness Testing of Aluminum Alloys*， 2024-04-19 Update
• ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*， 2024-04-19 Update
• ASTM B666/B666M-08 Standard Practice for Identification Marking of Aluminum and Magnesium Products*， 2024-04-19 Update
• ASTM E399-09 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials*， 2024-04-19 Update
• SAE AMS2355 TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
• SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)
• SAE ARP823 MINIMIZING STRESS CORROSION IN WROUGHT HEAT TREATABLE ALUMINUM ALLOY PRODUCTS
• SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4183A-2011 history

• 2016 SAE AMS4183A-2016 Aluminum Alloy, Extruded Profiles (2027-T3511) 4.4Cu - 1.2Mg - 0.8Mn - 0.10Zr Solution Heat Treated and Stress Relieved by Stretching
• 2011 SAE AMS4183A-2011 Aluminum Alloy, Extruded Profiles (2027-T3511) 4.4Cu 1.2Mg 0.8Mn 0.10Zr Solution Heat Treated and Stress Relieved by Stretching
• 2005 SAE AMS4183-2005 Aluminum Alloy, Extruded Profiles (2027-T3511) 4.4Cu 1.2Mg - 0.8Mn 0.10Zr Solution Heat Treated and Stress Relieved by Stretching UNS A92027