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Rivets, Nickel Alloy, Corrosion and Heat Resistant 47.5Ni-22Cr-1.5Co-9.0Mo-0.60W-18.5Fe Solution Heat Treated Procurement Specification For
- Aerospace Standard
- AS7237
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion and heat resistant nickel alloy of the type identified under the Unified Numbering System as UNS N06002.
Rationale
AS7237 has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | Material Composition | |
| TABLE 2 | Circular Runout Tolerance | |
| TABLE 3 | Rivet Driven Head Height | |
| TABLE 4 | Summary of Acceptance Tests | |
| TABLE 5 | Sampling Data |
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
| Number | Title |
|---|---|
| AMS2269 | Chemical Check Analysis Limits, Nickel, Nickel Alloys, and Cobalt Alloys |
| AMS2750 | Pyrometry |
| ASTME354 | This document is not part of the subscrption. |
| MIL-STD-1312 | This document is not part of the subscrption. |
| MIL-STD-2073-1 | This document is not part of the subscrption. |
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