Standard

SAE AIR4253A

Apr 2001 Withdrawn

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Language English

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Abstract

This information report (AIR) provides design information of various contemporary aircraft fly-by-wire (FBW) flight control actuation systems that may be useful in the design of future systems for similar applications. It is primarily applicable to manned aircraft. It presents the basic characteristics, hardware descriptions, redundancy concepts, functional schematics, and discussions of the servo controls, failure monitoring, and fault tolerance. All existing FBW actuation systems are not described herein; however, those most representing the latest designs are included. While this AIR is intended as a reference source of information for aircraft actuation system designs, the exclusion or omission of any other appropriate actuation system or subsystem should not limit consideration of their use on future aircraft.

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Standard from SAE International
Published: April 1 2001
Withdrawn: July 24 2018
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Replaced by: SAE AIR4253B
Replaces: SAE AIR4253

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Version history History (2)

SAE AIR4253A

SAE AIR4253

Abstract

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