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Studs, Installation Practice for Interference Fit - Metric
- Aerospace Standard
- MAP1670
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Scope
This document provides a recommended practice for installation of interference fit studs into threaded holes in non-ferrous alloys such as aluminum or magnesium.
Rationale
This document has been reaffirmed to comply with the SAE 5-year Review policy.
Recommended Content
| Aerospace Material Specification | Studs, Low-Alloy Steel Heat Treated, Rolled Threaded (Uns G87400) |
| Ground Vehicle Standard | Dryseal Pipe Threads |
| Aerospace Standard | Nuts, Self-Locking, Nickel Alloy, UNS N07001 Classification: 180 ksi/1400 °F Procurement Specification |
Data Sets - Support Documents
No Datasets Available
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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