SAE AIR 4253B:2018-07-24

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.

Author	SAE
Editor	SAE
Document type	Standard
Format	File
Cancellation date	2018-07-24
Confirmation date	2018-07-24
ICS	49.045 : Structure and structure elements
Number of pages	160
Replace	SAE AIR 4253A:2001-04-01
Replaced by	SAE AIR 4253B (2018-07-24)
Set	AEROPAKS10U-10
Year	2018
Document history	SAE AIR 4253A:2001-04-01
Country	USA
Keyword	SAE 4253;SAE AIR4253B;SAE AIR4253B;SAE AIR 4253