Browse Standards AIR1810A
Historical Reaffirmed 1991-06-01

Design, Development and Test Criteria-Solid State Proximity Switches/Systems for Landing Gear Applications AIR1810A

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 prosimity 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.
AIR1810C
2013-10-25
Latest
Reaffirmed
AIR1810B
2001-10-01
Historical
Revised
AIR1810A
1991-06-01
Historical
Reaffirmed
AIR1810
1983-09-01
Historical
Issued

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