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Studs, Steel, Low Alloy Heat Treated, Roll Threaded
- Aerospace Standard
- AS7456
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125 000 psi to 185 000 psi.
Rationale
This document has been reaffirmed to comply with the SAE 5-year Review policy.
Recommended Content
| Technical Paper | Developing High-Strength in a Deep Drawing Steel by a Post-Cold Rolling Nitriding Treatment |
| Aerospace Standard | Studs, Steel, Low Alloy Heat Treated, Roll Threaded |
Topic
Data Sets - Support Documents
No Datasets Available
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.
Reference
| Number | Title |
|---|---|
| AMS2640 | Magnetic Particle Inspection |
| AMS2750 | PYROMETRY |
| AMS6322 | STEEL .5 Ni .5 Cr .25 Mo (.38 - .43 C) |
| AMS6327 | STEEL .5 Ni .5 Cr .25 Mo (.38 - .43 C) (125,000 T.S.) |
| ANSI/ASME/B46.1 | This document is not part of the subscrption. |
| AS3062 | BOLTS, SCREWS AND STUDS, SCREW THREAD REQUIREMENTS |
| AS3063 | BOLTS, SCREWS AND STUDS, STRAIGHTNESS, CONCENTRICITY, AND SQUARENESS REQUIREMENTS |
| ASTME8 | This document is not part of the subscrption. |
| MIL-S-8879 | This document is not part of the subscrption. |
| MIL-STD-105 | This document is not part of the subscrption. |
| MIL-STD-1312 | This document is not part of the subscrption. |
| MIL-STD-2073-1 | This document is not part of the subscrption. |
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