SAE AMS-A-22771C-2012
Aluminum Alloy Forgings, Heat Treated

Standard No.
SAE AMS-A-22771C-2012
Release Date
2012
Published By
Society of Automotive Engineers (SAE)
Latest
SAE AMS-A-22771C-2012
Scope
This specification has previously been widely used and may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend this specification for future use in new designs. This specification covers the requirements for heat treated aluminum alloy die forgings, hand forgings, and ring forgings, produced under additional mechanical property control to ensure known mechanical properties for parts used in aerospace critical applications. This specification also covers the requirements for forgings furnished in the F or 01 conditions which will ultimately be used in the heat treated condition.

SAE AMS-A-22771C-2012 Referenced Document

  • ASTM B660-08 Standard Practices for Packaging/Packing of Aluminum and Magnesium Products*2024-04-20 Update
  • ASTM E1417-05 Standard Practice for Liquid Penetrant Testing*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 AMS-STD-2154-1998 Inspection, Ultrasonic, Wrought Metals, Process for
  • SAE AMS2355 TENSILE TESTING OF WROUGHT ALUMINUM AND MAGNESIUM PRODUCTS Except Forgings
  • SAE AMS2430 SHOT PEENING
  • SAE AMS2644-1996 Inspection Material@ Penetrant
  • SAE AMS2658 HARDNESS AND CONDUCTIVITY INSPECTION OF HEAT TREATED ALUMINUM ALLOY PARTS
  • SAE AMS2772-1997 Heat Treatment of Aluminum Alloy Raw Materials (01 1997)

SAE AMS-A-22771C-2012 history




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