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SAE AIR4253 Rev B

Description of Actuation Systems for Aircraft With Fly-By-Wire Flight Control Systems
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SAE AIR4253 Rev B

Description of Actuation Systems for Aircraft With Fly-By-Wire Flight Control Systems

PUBLISH DATE 2012
PAGES 160
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This SAE Aerospace 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.
SDO SAE: SAE International
Document Number AIR4253
Publication Date Aug. 10, 2012
Language en - English
Page Count 160
Revision Level B
Supercedes
Committee
Publish Date Document Id Type View
Aug. 10, 2012 AIR4253B Revision
April 1, 2001 AIR4253A Revision
April 28, 1989 AIR4253 Revision