SAE AIR1810A-1991
DESIGN, DEVELOPMENT AND TEST CRITERIA - SOLID STATE PROXIMITY SWITCHES/SYSTEMS FOR LANDING GEAR APPLICATIONS

Standard No.

SAE AIR1810A-1991

Release Date

1991

Published By

Society of Automotive Engineers (SAE)

Status

Be replaced 2001-12

Replace By

SAE AIR1810B-2001

Latest

SAE AIR1810D-2023

Scope

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.

SAE AIR1810A-1991 history

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