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SAE - SAE AS8584 - BRAKE SYSTEMS, WHEEL, MILITARY AIRCRAFT Organization: SAE
Date: 2013-11-01
Description: This SAE Aerospace Standard (AS) defines the requirements for brake systems used on military aircraft equipped with wheel-type landing gears. Product Classification Brake systems shall be either mechanical, hydraulic, pneumatic, electric or a combination of each.
SAE - SAE ARP1311 - (R) LANDING GEAR STRUCTURES AND MECHANISMS Organization: SAE
Date: 2009-02-01
Description: This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft. All axles, wheel forks, links, arms, mechanical and gas/oil shock struts, downlock and uplock assemblies, braces, trunnion beams, and truck beams etc., that sustain loads originating at the ground, and that are not integral parts of the airframe structure, should be designed and validated in accordance with this document.
SAE - SAE ARP1786 - (R) WHEEL ROLL ON RIM CRITERIA FOR AIRCRAFT APPLICATIONS Organization: SAE
Date: 2013-09-01
Description: Purpose This SAE Aerospace Recommended Practice (ARP) is to provide a recommended minimum laboratory roll performance for main landing gear aircraft wheels without tires installed and applies to both bolted and lock-ring wheel designs for FAA Part 25 and military aircraft main wheels (not required for any nose wheels or main wheels on FAA Part 23, 27 or 29 applications).
SAE/TP - 2010-01-1744 - AN ELECTROMECHANICALLY ACTUATED NOSE LANDING GEAR USING A DUAL-OUTPUT MOTOR CONTROL UNIT Organization: SAE/TP
Date: 2010-11-02
Description: This paper describes the design, construction and testing of a dual-output power converter concept where the large components, such as the DC link capacitor and heat-sink, are shared between two actuators which are used sequentially in the deployment of aircraft landing gear. This mutual component approach combines the advantages of dual-use power converters with the flexibility of one power converter per application.
SAE - SAE AS5663 - MINIMUM PERFORMANCE REQUIREMENTS FOR TRANSPORT AIRPLANE WHEEL AND BRAKE ASSEMBLIES USING ELECTRIC POWER ACTUATION Organization: SAE
Date: 2012-07-01
Description: This document does not address qualification of the EMAs or brake assembly to the landing gear environmental threats including, but not limited to, EMI/HIRF, failure mode operation or other application specific performance, or the qualification of software or of complex custom micro-coded components, including but not limited to, Programmable Logic Devices (PLD) and Application Specific Integrated Circuits (ASIC).
SAE/TP - 2009-01-3110 - DRESS: DISTRIBUTED AND REDUNDANT ELECTRO-MECHANICAL NOSE WHEEL STEERING SYSTEM Organization: SAE/TP
Date: 2009-11-10
Description: Scope of the DRESS project is to research, develop and validate a distributed and redundant electrical steering system technology for an aircraft nose landing gear. The new system aims to: • reduce system weight at aircraft level, replacing the current hydraulic actuation system with an electric one.
GMNA - 9986177 - FLUID, MANUAL TRANSMISSION, SYNTHETIC - ISSUE 2 Organization: GMNA
Date: 2014-12-01
Description: A synthetic manual transmission lubricant intended for use in Front Wheel Drive (FWD) vehicles. This material would be classified as SAE 75W-80 and American Petroleum Industry (API) Gear Lubricant (GL) API GL-4.
SAE - SAE ARP5600 - DISPOSITION OF DAMAGED WHEELS INVOLVED IN ACCIDENTS/INCIDENTS Organization: SAE
Date: 2005-05-01
Description: This SAE Aerospace Recommended Practice (ARP) establishes a procedure for disposition of aircraft wheels that have been involved in accidents/incidents or have been exposed to overheat conditions or overload conditions from loss of adjacent tire pressure (paired wheels) or wheel tie bolts. Recommendations in this document apply to main landing gear (braked) and nose landing gear aircraft wheels, manufactured from aluminum forgings or castings.
SAE - SAE ARP1348 - BAGGAGE/CARGO TRAILER REQUIREMENTS Organization: SAE
Date: 2011-12-01
Description: This SAE Aerospace Recommended Practice (ARP) applies to airline trailer equipment with four wheel running gear pulled and steered through an integral tow bar, for use on airport ramps and other airport areas for transporting baggage, freight, and other materials.
SAE - SAE ARP6152 - AIRCRAFT TIRES SERVICE OVERLOAD CAPABILITY Organization: SAE
Date: 2012-12-01
Description: This SAE Aerospace Recommended Practice (ARP) defines a procedure for demonstrating service overload capability for new, main and nose landing gear, radial or bias tires fitted on multiple wheel landing gear of Part 25 certified aircraft.
SAE - SAE ARP6137 - TIRE PRESSURE MONITORING SYSTEMS (TPMS) FOR AIRCRAFT Organization: SAE
Date: 2010-08-01
Description: These guidelines include, but are not limited to: a) Design recommendations for system components, which: 1. monitor tire inflation, and, 2. are located in/on the tire/wheel assembly, landing gear axle, and/or aircraft avionics compartment.
SAE - SAE AIR5937 - INFORMATION ON ELECTRIC BRAKES Organization: SAE
Date: 2007-03-01
Description: Details on the design and control of electric motors, gear train design, ball or roller screw selection are available in the reference documents and elsewhere, but are outside the scope of this document.
SAE - SAE J1903 - (R) AUTOMOTIVE ADAPTIVE DRIVER CONTROLS, MANUAL Organization: SAE
Date: 1997-07-01
Description: 1.3.1.2 Group B--Those controls, operated by the driver, which are essential to the coordinated and safe operation of the vehicle in traffic situations. This includes ignition/starter switch, gear selector, parking brake, turn indicator lever, hazard flasher, horn, wiper/washer, defroster control, mirror, and headlight dimmer.

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