SAE AIR 1810C:2003

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

Published By	Publication Date	Number of Pages
SAE	2003-01-08	17

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Categories: 31.200 - Integrated circuits. Microelectronics, 33.100 - Electromagnetic compatibility (EMC), 43.040.10 - Electrical and electronic equipment, SAE

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Description

This document examines the most important considerations relative to the use of proximity sensing systems for applications on aircraft landing gear. In general, the recommendations included are applicable to other demanding aircraft sensor installations where the environment is equally severe.

Additional information

Published Code	SAE
Published By	SAE International, formerly Society of Automotive Engineers
Publication Date	2003-01-08
Pages Count	17
Language	English
Descriptors	Electronic control systems; Electromagnetic compatibility; Landing gear; Fault detection; Sensors and actuators; Mountings; Electronic equipment; Wheel wells; Integrated circuits; Failure modes and effects analysis
File Size	870.4 KB
ICS Codes	31.200 - Integrated circuits. Microelectronics 33.100 - Electromagnetic compatibility (EMC) 43.040.10 - Electrical and electronic equipment

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SAE AIR 1810C:2003

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