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PROPELLER SHAFT END - FLANGED 5.125(130.175) BOLT CIRCLE
- Aerospace Standard
- AS1414
- Reaffirmed
Sector:
Issuing Committee:
Language:
English
Rationale
AS1414 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
-
1
DATUM
IS ROTATIONAL AXIS OF SHAFT: I.E., THE COMMON AXIS OF THOSE SHAFT FEATURES ON WHICH THE SHAFT MOUNTS AND ROTATES: E.G., SPLINES, JOURNALS, ETC. -
2
BREAK SHARP EDGES .003–.015 (0.08 – 0.38) UNLESS OTHERWISE SPECIFIED.
-
3
SURFACE TEXTURE: ANSI B46.1-1962. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES (3.2 MICROMETRES).
-
4
DIMENSIONS IN INCHES (MILLIMETRES). METRIC CONVERSIONS ARE INTERNATIONAL SYSTEM UNITS (SI).
-
5
DIMENSIONING AND TOLERANCING: ANSI Y14.5-1973.
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6
THIS IS A DESIGN STANDARD. NOT TO BE USED AS A PART NUMBER.
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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
| Number | Title |
|---|---|
| ANSI/B46.1 | This document is not part of the subscrption. |
| ANSI/Y14.5 | This document is not part of the subscrption. |
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