SAE AS7471C
Bolts and Screws, Nickel Alloy, Uns N07001 Tensile Strength 165 Ksi, Corrosion and Heat Resistant Procurement Specification.
Standard:
AKA:
- AS7471
- Revision: C
- 2006-01-13
- Historical. Access the latest revision: AS7471F
- E-25 General Standards For Aerospace And Propulsion Systems
This procurement specification covers 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 N07001. The following specification designations and their properties are covered:AS7471165 ksi minimm ultimate tensile strength at room temperature.75 ksi stress-rupture strength at 1350 °F.105 ksi tension to 10.5 ksi tension fatigue at room temperature.AS7471-1165 ksi minimm ultimate tensile strength at room temperature.99 ksi minimum ultimate shear strength at room temperature.
History:| Standard | Published | Revision | Status |
|---|---|---|---|
| AS7471F | 2013-01-15 | Latest | |
| AS7471E | 2009-07-16 | Historical | |
| AS7471D | 2007-08-29 | Historical | |
| AS7471C | 2006-01-13 | Historical | |
| AS7471B | 1997-07-01 | Historical | |
| AS7471A | 1995-09-01 | Historical |
- SAE AS 7471
- Aerospace
- Nickel
- Parts
- Gas turbines
- Hybrid engines
- Jet engines