This specification covers an aluminum alloy in the form of plate. This plate has been used typically for aerospace structural parts requiring strength similar to that of 7475-T7351 but having 4% lower nominal density, but usage is not limited to such applications. Material is delivered in T34 temper and precipitation heat treated to obtain T82 temper by the end user.
SAE AMS4472-2011 Referenced Document
ASTM B594-09 Standard Practice for Ultrasonic Inspection of Aluminum-Alloy Wrought Products for Aerospace Applications*， 2024-04-19 Update
ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*， 2024-04-19 Update
ASTM B666/B666M-08 Standard Practice for Identification Marking of Aluminum and Magnesium Products*， 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)