This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
BOLT, MACHINE - HEXAGON HEAD, DRILLED 6 HOLES, PD SHANK, UNS S66286, .5625-18 UNJF-3A
- Aerospace Standard
- AS3120B
- Revised
Downloadable datasets available
This content contains a 2D/3D
configurator
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Rationale
FIGURE 1 REDRAWN, REVISE LEAD THREAD CHAMFER AND DRILLED HOLE POSITION REQUIREMENTS TO CONFORM TO AS1132, REVISE RANGE OF PART NUMBERS ALLOWING SUBSTITUTE DATUM IN NOTE 2, CORRECT ACROSS POINTS DIMENSION, ADD NEW NOTE FOR DISPOSITION OF EXISTING INVENTORY, UPDATE REFERENCE FOR FPI REQUIREMENTS, GENERAL EDITORIAL AND Y14.5M FORMAT CHANGES THROUGHOUT.
2D/3D Drawings
Some older browsers could require a plugin
install for 3D and or 2D previewer.
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE 1 | DIMENSIONS |
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
* 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.