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Bolts and Screws, Steel, UNS S66286 Classification: 130 ksi/1200 °F 1800 °F Solution Heat Treated, Aged After Roll Threaded Procurement Specification for
- Aerospace Standard
Published May 10, 2006 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable iron base alloy of the type identified under the Unified Numbering System as UNS S66286.
This document has been reaffirmed to comply with the SAE 5-year Review policy.
|Aerospace Standard||Bolts and Screws, Steel, UNS S66286 1650 °F Solution Heat Treated Precipitation Heat Treated Before Roll Threaded|
|Aerospace Standard||Studs, Steel, UNS S66286 Aged After Roll Threaded Procurement Specification For|
Data Sets - Support Documents
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|TABLE 1||UNJ External Thread Depth at 2H/3 and Allowable Thread Lap Depth|
|TABLE 2||Test Loads|
|TABLE 3||Summary of Acceptance Tests|
|TABLE 4||Sampling Data|
|TABLE 5||Classification of Visual and Dimensional Characteristics|
|TABLE 6||Sampling Data|
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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