This specification covers an aluminum alloy in the form of plate. This plate has been used typically for parts requiring a high level of mechanical properties and moderate resistance to exfoliation corrosion, but usage is not limited to such applications. Certain design and processing may cause this plate to become susceptible to stress-corrosion cracking: ARP 823 recommends practices to minimize such conditions.
SAE AMS4306B-2007 Referenced Document
ASTM B594-06 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 2024-04-18 Update
ASTM B645-02 Standard Practice for Plane-Strain Fracture Toughness Testing of Aluminum Alloys*， 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 B666/B666M-01 Standard Practice for Identification Marking of Aluminum and Magnesium Products*， 2024-04-18 Update
ASTM E1304-97 Standard Test Method for Plane-Strain (Chevron-Notch) Fracture Toughness of Metallic Materials
ASTM E602-03 Standard Test Method for Sharp-Notch Tension Testing with Cylindrical Specimens *， 2024-04-18 Update
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)