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STUD, LOCKED IN-RING LOCKED, SERRATED
- Aerospace Standard
- AS51989C
- Revised
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Language:
English
Rationale
FIGURE 1 RE-DRAWN, REVISE SHANK TO SERRATED COLLAR FILLET RADIUS, REVISE FILLET RADII ON STUD END AT BASE OF SERRATED COLLAR AND THREAD START (2 PLACES), ADD NEW VIEW X TO FIGURE 1, CLARIFY SHANK DIAMETER CALLOUT, RENUMBER NOTES, GENERAL EDITORIAL CHANGES.
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Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE 1 | FINE THREAD NUT END - COARSE THREAD STUD END | |
| TABLE 2 | FINE THREAD NUT END - FINE THREAD STUD END | |
| TABLE 3 | COARSE THREAD NUT END - COARSE THREAD STUD END | |
| TABLE 4 | COARSE THREAD NUT END - FINE THREAD STUD END | |
| TABLE 5 | TABULATED LENGTHS (NUT END) | |
| TABLE 6 | INTERCHANGEABILITY SEE NOTE 13 |
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
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