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Rivets, Carbon Steel Procurement Specification for
- Aerospace Standard
Published January 03, 2020 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This procurement specification covers aircraft-quality solid rivets and tubular end rivets made from a carbon steel of the type identified under the Unified Numbering System as UNS G10100.
This revision adds alternate hardness requirements for rivets less than 0.125 inch nominal diameter and additional testing procedures. It also adds a referee method for acceptance of small diameter rivets.
|Aerospace Standard||Rivets, Steel, Corrosion Resistant 18Cr-9Ni, Solution Heat Treated, Procurement Specification for|
|Aerospace Standard||Spring Pins, Tubular, Coiled Corrosion Resistant Nickel Base Alloy Procurement Specification For|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
|Table 1||Material composition|
|Table 2||Circular runout tolerance|
|Table 3||Rivet driven head height|
|Table 4A||Nondestructive tests|
|Table 4B||Destructive tests|
|Table 5||Sampling data, nondestructive tests, visual and dimensional|
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.
|AMS2259||Chemical Check Analysis Limits, Wrought Low-Alloy and Carbon Steels|
|AS125101||Rivet - 100° - Countersunk Head, Mild Steel|
|AS125551||RIVET - UNIVERSAL HEAD, MILD STEEL|
|ASTME18||This document is not part of the subscrption.|
|ASTME350||This document is not part of the subscrption.|
|MIL-STD-2073-1||This document is not part of the subscrption.|
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