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Studs, Corrosion and Heat Resistant Steel, UNS S66286 Tensile Strength 900 MPa, Procurement Specification, Metric FSC 5307
- Aerospace Standard
- MA3375D
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This document covers metric studs made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286. The following specification designations and their properties are covered:
Rationale
Section 2.2 definitions deleted, AS6416 added, Spec throughout document updated, sections 3.7.1.1, 3.7.2.1, and 3.7.2.3 changed, Figures 1 through 6 redrawn for clarity.
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Topic
Data Sets - Support Documents
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Table 1 | Test loads | |
Table 2 | MJ ext thread depth at 2H/3 and allowable thread lap depth | |
Table 3 | Summary of acceptance tests | |
Table 4 | Sampling data | |
Table 5 | Classification of visual and dimensional characteristics | |
Table 6 | Sampling data |
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
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