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CONES, REAR, PROPELLER HUB
- Aerospace Standard
- AS93D
- Reaf. Nonc.
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Rationale
THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY.
THE BEARING CONTACTS ON THE TAPER CONE SEAT SHALL BE EVENLY DISTRIBUTED AND SHALL COVER NOT LESS THAN 75 PERCENT OF THE BEARING AREA WHEN CHECKED TO AN APPROVED GAGE BY MINUTE BLUING PRIOR TO SPLITTING CONE
MAXIMUM TAPER ON A DIMENSION NOT TO EXCEED .0005 PER INCH OF LENGTH
BREAK SHARP EDGES .016 ±.010
MATERIAL: ALUM BRONZE AMS 4871
HARDNESS: BRINELL 200 MIN
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 |
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 |
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AMS4871 | ALUMINUM BRONZE CASTINGS Heat Treated |
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