SAE AMS4456-2012
Aluminum Alloy, Hand Forgings 8.0Zn 1.0Cu 1.6Mg 0.12Zr (7037-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged

Standard No.

SAE AMS4456-2012

Release Date

2012

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced

Replace By

SAE AMS4456A-2019

Latest

SAE AMS4456A-2019

Scope

This specification covers an aluminum alloy in the form of hand forgings 11 inches (280 mm) and under in nominal thickness, and of forging stock.

SAE AMS4456-2012 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 E399-09 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials*， 2024-04-19 Update
• ASTM G34-01 Standard Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test)*， 2024-04-19 Update
• ASTM G47-98 Standard Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum Alloy Products
• 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 AMS2808 IDENTIFICATION Forgings
• SAE AS1990-1990 Aluminum Alloy Tempers

SAE AMS4456-2012 history

• 2019 SAE AMS4456A-2019 Aluminum Alloy, Hand Forgings 8.0Zn - 1.0Cu - 1.6Mg - 0.12Zr (7037-T7452) Solution Heat Treated, Compression Stress Relieved, and Overaged
• 2012 SAE AMS4456-2012 Aluminum Alloy, Hand Forgings 8.0Zn 1.0Cu 1.6Mg 0.12Zr (7037-T7452) Solution Heat Treated, Compression Stress-Relieved, and Overaged