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TORQUE TIGHTENING THREADED FASTENERS
- Aerospace Standard
Published May 01, 1995 by SAE International in United States
Downloadable datasets availableAnnotation ability available
To supply information on recommended assembly torque limits for tension type nuts and bolts of the following materials and plating combinations given in Table I.
Data Sets - Support Documents
|TABLE I||Combinations of Fastener Materials|
|TABLE II||Assembly Torques for Self Locking Nuts|
|TABLE III||Combined Tensile Stress (f )|
|TABLE IV||Assembly Torques for Positioning Types Nuts (Plain Hex, Drld Hex, Castellated, etc.)|
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.
|MIL-L-7808||This document is not part of the subscrption.|
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