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Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications
- Aerospace Standard
- AIR1810C
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
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.
Rationale
AIR1810C has been reaffirmed to comply with the SAE five-year review policy.
Recommended Content
| Aerospace Standard | Landing Gear Switch Selection Criteria |
| Aerospace Standard | Aircraft Nosewheel Steering/Centering Systems |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 |
Issuing Committee
Reference
| Number | Title |
|---|---|
| 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. |
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