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

Reaffirmed

06/01/1991

Features
Issuing Committee
Scope
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR1810A
Pages
13
Citation
SAE International Information Report, DESIGN, DEVELOPMENT AND TEST CRITERIA - SOLID STATE PROXIMITY SWITCHES/SYSTEMS FOR LANDING GEAR APPLICATIONS, SAE Standard AIR1810A, Revised July 1986, Issued September 1983, https://doi.org/10.4271/AIR1810A.
Additional Details
Publisher
Published
Jun 1, 1991
Product Code
AIR1810A
Content Type
Information Report
Status
Reaffirmed
Language
English

Revisions