This specification covers an aluminum alloy in the form of plate. This product has been used in aerospace applications requiring a high level of mechanical properties and fractur thoughness, moderate resistance to stress-corrosion cracking and resistance to exfoliation corrosion, but usage is not limited to such applications.
SAE AMS4329A-2006 Referenced Document
ASTM B594-02 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 2024-04-18 Update
ASTM B594-06 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 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 G34-01 Standard Test Method for Exfoliation Corrosion Susceptibility in 2XXX and 7XXX Series Aluminum Alloys (EXCO Test)*， 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)