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.
SAE AIR1810-1983 history
1970SAE AIR1810D-2023 Installations/Applications, Development, and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications
2021SAE AIR1810C-2021 Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications
2003SAE AIR1810C-2003 (R) Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications
2001SAE AIR1810B-2001 Design@ Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications
1991SAE AIR1810A-1991 DESIGN, DEVELOPMENT AND TEST CRITERIA - SOLID STATE PROXIMITY SWITCHES/SYSTEMS FOR LANDING GEAR APPLICATIONS
1986SAE AIR1810A-1986 Design@ Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications
1983SAE AIR1810-1983 DESIGN, DEVELOPMENT AND TEST CRITERIA - SOLID STATE PROXIMITY SWITCHES/SYSTEMS FOR LANDING GEAR APPLICATIONS