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Limits and Fits - International Metric Tolerance System
- Aerospace Standard
- AIR1758A
- Stabilized
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This information report provides guidance when the ISO International metric tolerance system for limits and fits per ISO/R286 or ANSI B4.2-1978 is applied on a standard, and also provides a selected series of limits and fits for powerplant construction suitable for holes and shafts up to 500 mm. For holes or shafts over 500 mm or for limits and fits not shown, ISO/R286 should be consulted.
Rationale
This document has been determined to contain basic and stable technology which is not dynamic in nature.
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| TABLE I | Limits and Fits, International Metric Tolerance System, H7 h6 Assemblies | |
| TABLE II | Limits and Fits, International Metric Tolerance System, H7 g6 Assemblies | |
| TABLE III | Limits and Fits, International Metric Tolerance System, H6 n5 Assemblies |
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
| Number | Title |
|---|---|
| ANSI/B4.2 | This document is not part of the subscrption. |
| ISO/R1869 | This document is not part of the subscrption. |
| ISO/R1938 | This document is not part of the subscrption. |
| ISO/R286 | This document is not part of the subscrption. |
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