This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Insert, Screw Thread, Self-Locking, UNS S66286, Locked In, Key Locked Procurement Specification For
- Aerospace Standard
- AS4892A
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers inserts made from A286 alloy of the type identified under the Unified Numbering System as UNS S66286 which have self-locking internal threads and integrated locking keys to positively secure the insert against rotation when properly installed in threaded holes.
Rationale
AS4892A has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
Aerospace Standard | Insert, Screw Thread, Non-Locking, UNS S66286, Locked in, Key Locked Procurement Specification for |
Aerospace Standard | Stud, Locked In, Key Locked, UNS S66286, Classification: 140 ksi Procurement Specification For |
Aerospace Material Specification | Plating, Nickel-Cadmium Diffused |
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
Unnamed Dataset 4 | ||
TABLE 1 | INTERNAL THREAD SELF-LOCKING TORQUE | |
TABLE 2 | MINIMUM TENSILE STRENGTH | |
TABLE 3 | RESISTANCE TO PULLOUT FOR AS3545 INSERTS | |
TABLE 4 | RESISTANCE TO PULLOUT FOR AS3546 INSERTS | |
TABLE 5 | MINIMUM ROTATIONAL RESISTANCE REQUIREMENTS | |
TABLE 6 | THREAD HEIGHT | |
TABLE 7 | SUMMARY OF QUALIFICATION TESTS | |
TABLE 8 | SUMMARY OF ACCEPTANCE TESTS | |
TABLE 9 | SAMPLING DATA DESTRUCTIVE TESTS, MECHANICAL AND METALLURGICAL CHARACTERISTICS | |
TABLE 10 | SAMPLING DATA NON-DESTRUCTIVE TESTS, VISUAL AND DIMENSIONAL CHARACTERISTICS FOR CLASSES MAJOR A, MAJOR B, MINOR A, AND MINOR B | |
TABLE 11 | CLASSIFICATION OF VISUAL AND DIMENSIONAL CHARACTERISTICS |
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.