SAE AMSQQA250/22C
Aluminum Alloy, 7178-T76, Alclad Plate and Sheet Improved Exfoliation Resistant
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Standard by SAE International, 2014-02-14
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| AMSQQA250_22C.pdf |
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About This Item
This specification covers the specific requirements for improved exfoliation resistant alclad aluminum alloy 7178-T76 sheet and -T7651 plate. The general requirements are covered in AMS-QQ-A-250. The plate and sheet covered by this specification shall be an integral composite product consisting of a heat-treatable aluminum alloy (7178) core with thin layers of an aluminum alloy (7072) anodic to the core and of approximately equal thickness, bonded to both surfaces
AMS-QQ-A-250/22C has been designated stabilized because alloy 7178 is not recommended for new designs.
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Standard Details
- Publication Date: 2014-02-14
- Standard Status: latest
- Publisher: SAE International
- Document Type: Aerospace Material Specification
- Subject: Aluminum alloys, Conductivity, Tensile strength, Military aircraft, Humidity, Corrosion, Chemicals, Heat treatment, Composite materials
- Official SAE: Doi link
Document History
- This Version: AMSQQA250/22C (2014-02-14)
- Previous Version: AMSQQA250/22B (2012-04-04)
- Previous Version: AMSQQA250/22A (1998-09-01)
- Previous Version: AMSQQA250/22 (1997-08-01)
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