SAE ARP6252 PDF | Request Standard
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SAE ARP6252

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

Standard by SAE International, 2018-10-15

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  • Availability: Immediate Download
  • Language: English
  • License Type: Single User
  • Updates: Not Included
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  • Language: English
  • License Type: Enterprise / Multi User
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About This Item

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.
SKU: d8d16b58cccd

  • Publication Date: 2018-10-15
  • Standard Status: latest
  • Publisher: SAE International
  • Document Type: Aerospace Standard
  • Subject: Brake pedals, Flight control systems, Business and general aviation aircraft, Military aircraft, Commercial aircraft, Failure modes and effects analysis, Radio frequency, Lightning protection, Aircraft structures
  • Official SAE: Doi link

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