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STUD - STRAIGHT, DRILLED, .2500-20UNS X .2500-28UNF-3A
- Aerospace Standard
Published November 12, 2019 by SAE International in United States
Downloadable datasets available
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FIGURE REDRAWN, USAGE NOTE ADDED, SPECS UPDATED.
|Aerospace Material Specification||Aluminum Alloy, Bars, Rolled Or Cold Finished 1.0mg 0.60si 0.28cu 0.20cr Stress Relief Stretched|
|Aerospace Material Specification||Manganese Alloy, Brazing Filler Metal 66Mn - 16Ni - 16Co - 0.80B 1770 to 1875 °F (966 to 1024 °C) Solidus-Liquidus Range|
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Data Sets - Support Documents
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.
|AMS6322||STEEL .5 Ni .5 Cr .25 Mo (.38 - .43 C)|
|ANSI Y14.5M||This document is not part of the subscrption.|
|AS7456||Studs, Steel, Low Alloy Heat Treated, Roll Threaded|
|ASME B46.1||This document is not part of the subscrption.|
|ASME Y14.36M||This document is not part of the subscrption.|
|ASTME1444||This document is not part of the subscrption.|
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