This specification covers an aluminum alloy in the form of hand forgings 12 inches (305 mm) and under in nominal thickness and forging stock. These forgings have been used typically for machined structural parts and requiring high strength and resistance to stress-corrosion cracking, but usage is not limited to such application.
SAE AMS4414-2008 Referenced Document
ASTM B594-06 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 2024-04-18 Update
ASTM B645-07 Standard Practice for Linear-Elastic Plane-Strain Fracture Toughness Testing of Aluminum Alloys*， 2024-04-18 Update
ASTM B660-02 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*， 2024-04-18 Update
ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*， 2024-04-18 Update
ASTM E399-06 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials
ASTM E399-08 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness K Ic of Metallic Materials*， 2024-04-18 Update
ASTM G47-98 Standard Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum Alloy Products
SAE AMS2355H-2005 Quality Assurance Sampling and Testing of Aluminum Alloys and Magnesium Alloys, Wrought Products, Except Forging Stock, and Rolled, Forged, or Flash Welded Rings
SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)