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Nuts, Self-Locking, Alloy, Corrosion and Heat Resistant High Strength, All Metal, Dry Film Lubricated, 1400 °F (760 °C), Procurement Specification
- Aerospace Standard
- AS4417
- 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
This document has been reaffirmed to comply with the SAE 5-year Review policy.
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| 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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