This specification covers an aluminum alloy in the form of plate. This product may be used in aerospace applications requiring a high level of mechanical properties and fracture toughness, good resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.
SAE AMS4470A-2012 Referenced Document
ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 2024-04-20 Update
ASTM B645-10 Standard Practice for Linear-Elastic Plane-Strain Fracture Toughness Testing of Aluminum Alloys*， 2024-04-20 Update
ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*， 2024-04-20 Update
ASTM B666/B666M-08 Standard Practice for Identification Marking of Aluminum and Magnesium Products*， 2024-04-20 Update
ASTM E399-09 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials*， 2024-04-20 Update
ASTM G34-01 Standard Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test)*， 2024-04-20 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)