Areas for Calculating Stress or Load Values for Metric MJ Externally Threaded Fasteners
- Aerospace Standard
Area for ultimate shear stress or load in unthreaded shank.
Area for ultimate tensile stress or load in thread.
Area for stress durability test load in thread.
Area for stress-rupture test load at elevated temperature.
Area for tension-tension fatigue test load.
|Aerospace Material Specification||Insulation, Electrical, Pasted-Mica|
|Aerospace Standard||BRACKET, ANGLE, 90° .190 X .375 BOLT|
|Aerospace Material Specification||Steel Plate 2.0Cr - 10Ni - 14Co - 1.0Mo (0.13 - 0.17C) Vacuum Melted, Normalized, and Overaged|
Data Sets - Support Documents
|TABLE 1||Areas for Externally Threaded Fasteners with Metric MJ Thread, mm|
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.
|MA1370||Screw Threads - MJ Profile, Metric|