AIR4253B Description of Actuation Systems for Aircraft With Fly-By-Wire Flight Control Systems

Reaffirmed

07/24/2018

Features
Issuing Committee
Scope
Content
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.
Rationale
Content
The purpose of revision B of this document is to expand its scope to add descriptions of the flight control actuation systems for additional aircraft developed recently. Those new aircraft are the A380, Eurofighter, BA609 Tiltrotor and A400M.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR4253B
Pages
160
Citation
SAE International Information Report, Description of Actuation Systems for Aircraft With Fly-By-Wire Flight Control Systems, SAE Standard AIR4253B, Reaffirmed July 2018, Revised August 2012, Issued April 1989, https://doi.org/10.4271/AIR4253B.
Additional Details
Publisher
Published
Jul 24, 2018
Product Code
AIR4253B
Content Type
Information Report
Status
Reaffirmed
Language
English

Revisions