SAE AS7467
BOLTS AND SCREWS, NICKEL ALLOY, CORROSION AND HEAT RESISTANT Forged Head, Roll Threaded, Stress-Rupture Rated
Historical
Standard by SAE International, 1991-01-22
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| AS7467.pdf |
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About This Item
This procurement specification covers aircraft quality bolts and screws made from a corrosion and heat resistant age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07718 and of 185 000 psi tensile strength at room temperature, with maximum test temperature of parts at 1200°F.
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Standard Details
- Publication Date: 1991-01-22
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Standard
- Subject: Corrosion resistant alloys, Heat resistant materials, , , , , , ,
- Official SAE: Doi link
Document History
- New Version Available: AS7467C (2021-04-19)
- Previous Version: AS7467B (2013-06-27)
- Previous Version: AS7467A (2006-05-08)
- This Version: AS7467 (1991-01-22)
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