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Control Lever Connections (60° V Serrations)
- Aerospace Standard
Published April 28, 2018 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Recommended Practice (ARP) provides the definition for a control lever connection with 60° "V" serrations for aircraft engine to aircraft power or control levers.
This document has been determined to contain basic and stable technology which is not dynamic in nature.
|SAE ITC E&A Standard||AS2227 Rivet, Snap Head|
|Aerospace Material Specification||Felt, Firm Pad, White 100% Wool|
Data Sets - Support Documents
|Unnamed Dataset 1|
|TABLE 1||Performance and Assembly Data|
|TABLE 2||Clearance Diameter Versus Thread Size|
|TABLE 3||Serration Data for at .750 OD Unless Otherwise Specified|
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.
|ANSI/B46.1||This document is not part of the subscrption.|
|MIL-S-7742||This document is not part of the subscrption.|
|MIL-S-8879||This document is not part of the subscrption.|
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