This Aerospace Recommended Practice (ARP) provides general requirements for a generic, integrated rudder and brake pedal unit, incorporating a passive force-feel system that could be used for fixed-wing fly-by wire transport and business aircraft. This ARP addresses the following: The functions to be implemented The mechanical interconnection between captain and F/O station The geometric and mechanical characteristics The mechanical, electrical, and electronic interfaces The safety and certification requirements There is a need for a document that provides general requirements for an integrated rudder and brake pedal unit based on a passive force-feel system that could be used interconnected with a similar unit for the adjacent pilot. This is because, increasingly, commercial fixed-wing transport and business aircraft are using fly-by wire flight control systems and the OEMs wish to control them with integrated rudder and brake pedal inceptor units, rather than the mechanism and sub-assemblies previously used. This document satisfies this need.


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    Title :

    Integrated Rudder and Brake Pedal Unit, General Requirements for Fly-By Wire Transport and Business Aircraft


    Publication date :

    2018-10-15



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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