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Performance, Nut, Self-Locking, Castellated, Prevailing Torque, UNJ 16 Pitch Thread Form
- Aerospace Standard
Published May 04, 2006 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document covers all metal, castellated, self-locking nuts made from alloy steel of the types identified under the Unified Numbering System as UNS G41300 and UNS G43400.
This document has been reaffirmed to comply with the SAE 5-year Review policy.
|Ground Vehicle Standard||Torque-Tension Test Procedure for Steel Threaded Fasteners - Metric Series|
|Technical Paper||Corrosion and Safety|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|TABLE 1||Locking Feature Torques|
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.
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