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SAE International - AS8584A

Brake Systems, Wheel, Military Aircraft

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Organization: SAE International
Publication Date: 20 October 2008
Status: active
description:

This SAE Aerospace Standard (AS) defines the requirements for brake systems used on military aircraft equipped with wheel-type landing gears.

Document History

AS8584A
October 20, 2008
Brake Systems, Wheel, Military Aircraft
This SAE Aerospace Standard (AS) defines the requirements for brake systems used on military aircraft equipped with wheel-type landing gears.

References

This document references:
AIR5372 - Information on Brake-By-Wire (BBW) Brake Control Systems
Published by SAE International on April 22, 2013
A panel of the SAE A-5A Committee prepared this SAE Aerospace Information Report (AIR). The document describes the design approaches used for current applications of Brake-by-Wire (BBW) control...
This document references:
ARP1070 - DESIGN OF AIRCRAFT SKID CONTROL SYSTEMS FOR COMPATIBILITY WITH AIRPLANE EQUIPMENT
Published by SAE International on April 1, 1969
A description is not available for this item.
This document references:
ARP1493 - WHEEL & BRAKE DESIGN AND TEST REQUIREMENTS FOR MILITARY AIRCRAFT
Published by SAE International on July 1, 1979
A description is not available for this item.
This document references:
AS22759 - Wire, Electrical, Fluoropolymer-Insulated, Copper or Copper Alloy
Published by SAE International on July 1, 2001
This specification covers fluoropolymer-insulated single conductor electrical wires made with tin-coated, silver-coated, or nickel-coated conductors of copper or copper alloy as specified in the...
This document references:
AS50881 - WIRING, AEROSPACE VEHICLE
Published by SAE International on April 1, 1998
This specification covers all aspects from the selection through installation of wiring and wiring devices used in aerospace vehicles. Aerospace vehicles include airplanes, helicopters,...
This document references:
AS5440 - Hydraulic Systems, Aircraft, Design and Installation Requirements For
Published by SAE International on April 1, 1998
This specification covers the design and installation requirements for Types I and II aircraft hydraulic systems.
This document references:
AS8775 - Hydraulic System Components, Aircraft and Missiles, General Specification For
Published by SAE International on November 17, 2008
This specification covers the general requirements that are common to most hydraulic components (see 6.2 ), used in aeronautical hydraulic systems (see 6.1 ).
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