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Bolts and Screws, Steel, Low-Alloy Heat-Resistant 220,000 psi (1517 MPa) Tensile Strength Hardened and Tempered, Roll Threaded
- Aerospace Material Specification
- AMS7464C
- Reaf. Nonc.
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification covers premium quality bolts and screws made from a low-alloy, heat-resistant steel and having threads of UNJ (MIL-S-8879) form.
Rationale
This document has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
| Aerospace Material Specification | Bolts and Screws, Steel, Low-Alloy Heat Resistant 222,000 psi (1517 MPa) Tensile Strength Hardened and Tempered, Roll Threaded |
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Topic
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| TABLE II | (SI) |
Issuing Committee
E-25 General Standards for Aerospace and Propulsion Systems
The SAE E-25 General Standards for Aerospace & Propulsion Systems committee addresses aerospace propulsion systems and components. These systems and components include bolts, screws, nuts, washers, studs, rivets, pins, covers, O-rings, brackets, plugs and associated procurement requirements, as well as solid film lubricants and design specifications for screw threads and fastener assembly requirements.
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