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Studs, Corrosion and Heat Resistant Steel, UNS S66286 Tensile Strength 900 MPa, Procurement Specification, Metric
- Aerospace Standard
- MA3375C
- 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
To revise paragraph 3.6 by adding “two to” three threads in agreement with NASM1312 test methodology and general updating of specifications and SAE formatting requirements.
Recommended Content
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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