Standard

SAE AMS-QQ-A-250/22C

Published

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Abstract

This alloy is intended for use where high strength is required and where exfoliation and stresscorrosion resistance superior to 7178-T6 is required in high performance military aircraft.

Document information

  • Standard from SAE_AC
  • Published:
  • Version: 0
  • Document type: IS
  • Additional information
  • (Composition similar to UNS A87178)