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SLEEVE, REMOVABLE SELF-LOCKING NUT, UNS S30403
- Aerospace Standard
Published May 03, 2006 by SAE International in United States
Downloadable datasets availableAnnotation ability available
THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY.
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.
|AMS5511||STEEL, SHEET AND STRIP - CORROSION AND HEAT RESISTANT 18Cr - 8Ni Extra Low Carbon|
|AMS5647||STEEL, CORROSION RESISTANT 18Cr - 8Ni (304L)|
|ANSI/ASME/B46.1||This document is not part of the subscrption.|
|ANSI/Y14.36||This document is not part of the subscrption.|
|ANSI/Y14.5M||This document is not part of the subscrption.|
|AS3550||ASSEMBLY NUT, PLATE, REMOVABLE SELF-LOCKING NUT|
|FED-QQ-P-35||This document is not part of the subscrption.|
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