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NUTS, SELF-LOCKING, NICKEL ALLOY, UNS N07001 180 000 psi, ALL METAL 1400 °F USE, UNJ THREAD FORM
- Aerospace Standard
Published December 23, 1991 by SAE International in United States
This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made of a corrosion and heat resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001. Axial tensile strength 180 000 psi at room temperature. Maximum test temperature of parts is 1400 °F.
|Aerospace Material Specification||Iron Alloy, Corrosion and Heat Resistant, Covered, Welding Electrodes 31Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0 (Cb + Ta)|
|Aerospace Material Specification||Tantalum Sheet, Strip, and Plate Annealed|
|Aerospace Material Specification||Flux, Aluminum Dip Brazing 1030 °F (554 °C) or Lower Liquidus|
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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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