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SAE AIR 1810C:2013-10-25
New product
SAE AIR 1810C:2013-10-25
Design, Development and Test Criteria - Solid State Proximity Switches/Systems for Landing Gear ApplicationsMore info
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.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2013-10-25 |
| ICS | 49.045 : Structure and structure elements
|
| Number of pages | 17 |
| Replace | SAE AIR 1810B:2001-10-01 |
| Set | AEROPAKS10U-10 |
| Year | 2013 |
| Document history | SAE AIR 1810B:2001-10-01 |
| Country | USA |
| Keyword | SAE 1810;SAE AIR1810C;SAE AIR1810C;SAE AIR 1810 |