This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
AREAS FOR CALCULATING STRESS OR LOAD VALUES FOR METRIC MJ EXTERNALLY THREADED FASTENERS
- Aerospace Standard
- AS1520
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
Areas for the standard metric series of thread diameter-pitch combinations for aerospace externally threaded fasteners are established for the following conditions:
-
a)
Area for ultimate shear stress or load in unthreaded shank.
-
b)
Area for ultimate tensile stress or load in thread.
-
c)
Area for stress durability test load in thread.
-
d)
Area for stress-rupture test load at elevated temperature.
-
e)
Area for tension-tension fatigue test load.
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE I | Areas for Externally Threaded Fasteners with Metric MJ Threads, mm |
Issuing Committee
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.
Reference
| Number | Title |
|---|
* Redlines comparisons are available for those standards
listed in the Revision History that contain a radio button. A
redline comparison of the current version against a revision is
accomplished by selecting the radio button next to the standard and
then selecting 'compare'. At this time, Redline versions only exist
for some AMS standards. SAE will continue to add redline versioning
with ongoing updates to SAE MOBILUS.