This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Wheel Roll on Rim Criteria for Aircraft Applications
- Aerospace Standard
Published February 15, 2019 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This SAE Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheels without tires installed and applies to both bolted and lock-ring wheel designs for FAA Part 25 and military aircraft main wheels (not required for any nose wheels or main wheels on FAA Part 23, 27 or 29 applications).
This document is intended to provide recommended practice for aircraft wheel roll on rim design criteria and validation test. This revision C is an update to revision B and incorporates an updated reference section.
|Aerospace Standard||Design and Verification of Aircraft Nose Wheel Steering Systems|
|Technical Paper||Aircraft Level Steering Runaway Failure Analysis|
Data Sets - Support Documents
|Unnamed Dataset 1|
|Unnamed Dataset 2|
* Redlines comparisons are available for those standards listed in the Revision History that contain a radio button. A redline comparison of the current version against a revision is accomplished by selecting the radio button next to the standard and then selecting 'compare'. At this time, Redline versions only exist for some AMS standards. SAE will continue to add redline versioning with ongoing updates to SAE MOBILUS.