SAE AIR 4922A:2015

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Primary Flight Control Hydraulic Actuation System Interface Definition

Published By	Publication Date	Number of Pages
SAE	2015-10-19	50

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Categories: 43.040.10 - Electrical and electronic equipment, SAE

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Description

This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed.

Additional information

Published Code	SAE
Published By	SAE International, formerly Society of Automotive Engineers
Publication Date	2015-10-19
Pages Count	50
Language	English
Descriptors	Failure modes and effects analysis; Flight control actuators; Fly-by-wire control systems; Flight control systems; Control systems; Fiber optics; Electronic equipment
File Size	2.6 MB
ICS Codes	43.040.10 - Electrical and electronic equipment

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SAE AIR 4922A:2015

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SAE AIR 4922A:2015

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