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Nuts, Self-Locking, Alloy, Corrosion and Heat Resistant, High Strength, All Metal, Solid Film Lubricated, 1400 °F, Procurement Specification
- Aerospace Standard
- AS4417A
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This document covers all-metal, self-locking nuts, plate nuts, and gang channel nuts made of a corrosion and heat resistant nickel alloy.
Rationale
Update thread specification to AS8879, add option for permanent set to test on bolt, revise coating allowance to AS8879 requirements, remove SI units throughout, update references throughout, general editorial update, redraw figures and re-format tables.
Recommended Content
Topic
Data Sets - Support Documents
Title | Description | Download |
---|---|---|
Unnamed Dataset 1 | ||
Unnamed Dataset 2 | ||
Unnamed Dataset 3 | ||
TABLE 1 | AXIAL TENSILE LOAD | |
TABLE 2 | FIRST CYCLE MINIMUM BREAKAWAY TORQUES | |
TABLE 3 | INSTALLATION, REMOVAL AND BREAKAWAY TORQUE LIMITS | |
TABLE 4 | TEST BOLT | |
TABLE 5 | SEATING TORQUE | |
TABLE 6 | VIBRATION TEST, ASSEMBLY TORQUE | |
TABLE 7 | PUSH-OUT | |
TABLE 8 | TORQUE-OUT |
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
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