SAE AIR1810A PDF
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DESIGN, DEVELOPMENT AND TEST CRITERIA – SOLID STATE PROXIMITY SWITCHES/SYSTEMS FOR LANDING GEAR APPLICATIONS
Description
This document will examine the more important considerations relative to the utilization of “one piece”, or integral electronics proximity switches, and “two piece”, or separate sensor and electronics proximity switches, for applications on aircraft landing gear. In general, the recommendations included are applicable for other demanding aircraft sensor installations where the environment is equally severe.
History
| AIR1810D | 2023-12-13 | Latest | Revised |
| AIR1810C | 2021-02-03 | Historical | Reaffirmed |
| AIR1810B | 2001-10-01 | Historical | Revised |
| AIR1810A | 1991-06-01 | Historical | Reaffirmed |
| AIR1810 | 1983-09-01 | Historical | Issued |
| ISSUING COMMITTEE | A-5B Gears, Struts and Couplings Committee |
|---|---|
| DATE | 1991-06-01 |
| DOI | |
| ISCURRENT | |
| PAGE | 13 |
| PUBLISHER | SAE International |
| REVISED | REVISED |
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