This content is not included in your SAE MOBILUS subscription, or you are not logged in.
Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications
- Aerospace Standard
Published February 03, 2021 by SAE International in United States
Downloadable datasets availableAnnotation ability available
This document examines the most important considerations relative to the use of proximity sensing systems for applications on aircraft landing gear. In general, the recommendations included are applicable to other demanding aircraft sensor installations where the environment is equally severe.
AIR1810C has been reaffirmed to comply with the SAE five-year review policy.
|Aerospace Standard||Landing Gear Switch Selection Criteria|
|Aerospace Standard||Aircraft Nosewheel Steering/Centering Systems|
Data Sets - Support Documents
|Unnamed Dataset 1|
|MIL-C-85049||This document is not part of the subscrption.|
|MIL-I-16923||This document is not part of the subscrption.|
|MIL-PRF-23586||This document is not part of the subscrption.|
|MIL-STD-461||This document is not part of the subscrption.|
|MIL-STD-704||This document is not part of the subscrption.|
|MIL-STD-810||This document is not part of the subscrption.|
|MIL-W-22759||This document is not part of the subscrption.|
|RTCA-DO-160||This document is not part of the subscrption.|
* 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.