【范围】
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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.strRefField
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