Standard

SAE AIR4253

May 1999 Withdrawn

Existing or new amendments and versions must be purchased separately.

Language English

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Abstract

This AIR provides a description of representative state-of-the-art, fly-by-wire (FBW) actuation systems used in flight control systems of 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 future 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.

Products specifications

Standard from SAE International
Published: May 1 1999
Withdrawn: April 1 2001
Document type: IS
Pages
ISBN:

Publisher: SAE International
Distributor: SAE International

Product Relations

Referred by: SAE AIR5273A
Referred by: SAE AIR4922A
Referred by: SAE AIR4922
Referred by: SAE AIR5273
Replaced by: SAE AIR4253A

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Abstract

Products specifications

Product Relations