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Flaring (Swaging) and Removal of Shank Nuts
- Aerospace Standard
- ARP4848
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
To specify the approved method of flaring the shank of self-locking shank nuts, and to provide the preferred method for removal of damaged nut.
Rationale
ARP4848 has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
| Aerospace Standard | Flaring (Swaging) and Removal of Shank Nuts |
| Technical Paper | Automatic Feeding of Temporary Fasteners in Confined Spaces |
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| TABLE 1 | Anvil Diameter | |
| TABLE 2 | Tool Dimensions, Alternative Flaring Method | |
| TABLE 3 | Tool Clearance Dimensions | |
| TABLE 4 | Recommended Drill Size (For AS3534 and AS3535 Shank Nuts) |
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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