SAE AS7468
BOLTS AND SCREWS, COBALT-CHROMIUM-NICKEL ALLOY, CORROSION RESISTANT Forged Head, Roll Threaded After Aging, Fatigue Rated
Historical
Standard by SAE International, 1991-01-17
Quick Links
Norma
Get answers for your technical
Standart Library
Find standards for your sector
Standart Chek
Verify updates for your standards
|
Name |
Available Formats |
Availability |
Language |
|---|---|---|---|
| AS7468.pdf |
Secure PDF |
Immediate Download | English |
| AS7468.pdf |
Online Access |
Request Quote | English |
Customers Who Bought This Also Bought
About This Item
This procurement specification covers aircraft quality bolts and screws made from a corrosion resistant, work-strengthened, cobalt-chromium-nickel alloy of the type identified under the Unified Numbering System as UNS R30035, and of 260 000 psi tensile strength at room temperature.
Please request information about the document. Contact Page
Standard Details
- Publication Date: 1991-01-17
- 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: AS7468C (2020-04-11)
- Previous Version: AS7468B (2012-11-19)
- Previous Version: AS7468A (1997-12-01)
- This Version: AS7468 (1991-01-17)
Please request information about the document. Contact Page
