AIR1810B Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications

Revised

10/01/2001

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/AIR1810B
Pages
14
Citation
SAE International Information Report, Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear Applications, SAE Standard AIR1810B, Revised October 2001, Reaffirmed June 1991, Issued September 1983, https://doi.org/10.4271/AIR1810B.
Additional Details
Publisher
Published
Oct 1, 2001
Product Code
AIR1810B
Content Type
Information Report
Status
Revised
Language
English

Revisions