SAE AIR 5273:2001

$25.35

Actuation System Failure Detection Methods

Published By	Publication Date	Number of Pages
SAE	2001-12-20	54

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Categories: 43.040.10 - Electrical and electronic equipment, SAE

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Description

This AIR provides descriptions of aircraft actuation system failure-detection methods. The methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight control. The AIR concentrates on full Fly-By-Wire (FBW) flight control actuation though it includes one augmented-control system. The background to the subject is discussed in terms of the impact that factors such as the system architecture have on the detection methods chosen for the flight control system. The types of failure covered by each monitoring technique are listed and discussed in general. The way in which these techniques have evolved is illustrated with an historical review of the methods adopted for a series of aircraft, arranged approximately in design chronological order.

Additional information

Published Code	SAE
Published By	SAE International, formerly Society of Automotive Engineers
Publication Date	2001-12-20
Pages Count	54
Language	English
Descriptors	Failure modes and effects analysis; Flight control actuators; Fly-by-wire control systems; Flight control systems; Safety critical systems; Electrical systems; Electronic equipment; Electronic control units; Control systems
File Size	655.4 KB
ICS Codes	43.040.10 - Electrical and electronic equipment

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SAE AIR 5273:2001

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