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Flaring (Swaging) and Removal of Shank Nuts
- Aerospace Standard
Published August 23, 2018 by SAE International in United States
Downloadable datasets availableAnnotation ability available
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.
ARP4848 has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Standard||Flaring (Swaging) and Removal of Shank Nuts|
|Technical Paper||Automatic Feeding of Temporary Fasteners in Confined Spaces|
Data Sets - Support Documents
|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)|
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.
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