• SAE ARP 1070 : 2014

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY

    Available format(s):  Hardcopy, PDF

    Superseded date:  24-07-2019

    Language(s):  English

    Published date:  01-01-2014

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. APPLICABLE DOCUMENTS
    3. ANTISKID, DESCRIPTION OF OPERATION
    4. ANTISKID SYSTEM DEVELOPMENT PROCESS
    5. AIRCRAFT SYSTEMS AND AIRCRAFT OPERATIONAL
       GOALS, EFFECT ON ANTISKID
    6. ANTISKID REQUIREMENTS
    7. COMPONENT TESTING AND EVALUATION
    8. SYSTEM LEVEL ANTISKID PERFORMANCE AND SAFETY
       TESTING AND EVALUATION
    9. NOTES

    Abstract - (Show below) - (Hide below)

    Describes the development process and makes recommendations for total antiskid/aircraft systems compatibility.

    General Product Information - (Show below) - (Hide below)

    Committee A-5A
    Development Note Supersedes SAE AS 483. (01/2011)
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    SAE ARP 1907 : 2016 AUTOMATIC BRAKING SYSTEMS
    SAE AIR 5800 : 2015 TIRE PREROTATION AT LANDING
    SAE AIR 5372 : 2014 INFORMATION ON BRAKE-BY-WIRE (BBW) BRAKE CONTROL SYSTEMS
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    SAE AIR 5937 : 2012 INFORMATION ON ELECTRIC BRAKES
    SAE ARP 5632 : 2016 ROTORCRAFT: APPLICATION OF EXISTING AIRCRAFT DESIGNED TIRES, WHEELS AND BRAKES

    Standards Referencing This Book - (Show below) - (Hide below)

    MIL B 8075 : D BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    SAE AMS QQ P 416 : 2016 PLATING, CADMIUM (ELECTRODEPOSITED)
    MIL-STD-704 Revision F:2004 AIRCRAFT ELECTRIC POWER CHARACTERISTICS
    MIL-STD-130 Revision N:2007 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY
    IEEE 12207.1-1997 IEEE/EIA Guide - Industry Implementation of International Standard ISO/IEC 12207 : 1995 (ISO/IEC 12207) - Software Life Cycle Processes - Life Cycle Data
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    SAE ARP 4955 A: 2012(R2018) RECOMMENDED PRACTICE FOR MEASUREMENT OF STATIC AND DYNAMIC CHARACTERISTIC PROPERTIES OF AIRCRAFT TIRES
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    NAS1638:2011 CLEANLINESS REQUIREMENTS OF PARTS USED IN HYDRAULIC SYSTEMS
    SAE AIR 1739 : 2016 INFORMATION ON ANTISKID SYSTEMS
    ARINC 629 : 90 SUPP 5 MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    FAA AC 20-152 : 2005 RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    MIL-HDBK-454 Revision B:2007 GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT
    FAA AC 23-8 : 2011 FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES
    ASME Y14.24 : 2012 TYPES AND APPLICATIONS OF ENGINEERING DRAWINGS - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    SAE AS 22759 : 2014 WIRE, ELECTRICAL, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY
    MIL-PRF-81322 Revision G:2005 GREASE, AIRCRAFT, GENERAL PURPOSE, WIDE TEMPERATURE RANGE, NATO CODE G-395
    MIL-STD-1568 Revision D:2015 Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems
    MIL-HDBK-5400 Base Document:1995 ELECTRONIC EQUIPMENT, AIRBORNE GENERAL GUIDELINES FOR
    MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
    MIL-STD-882 Revision E:2012 System Safety
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    IEEE 12207.0-1996 IEEE/EIA Standard - Industry Implementation of International Standard ISO/IEC 12207:1995 (ISO/IEC 12207) Standard for Information Technology -- Software Life Cycle Processes
    RTCA DO 248 : C2011 SUPPORTING INFORMATION FOR DO-178C AND DO-278A
    SAE AS 8775 : 1998 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES, GENERAL SPECIFICATION FOR
    SAE ARP 598 : 2016 AEROSPACE MICROSCOPIC SIZING AND COUNTING OF PARTICULATE CONTAMINATION FOR FLUID POWER SYSTEMS
    MIL-DTL-26500 Revision G:2011 CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING OR HERMETICALLY SEALED, GENERAL SPECIFICATION FOR
    FAA AC 25-7 : 2012 FLIGHT TEST GUIDE FOR CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES
    SAE ARP 490 : 2008 ELECTROHYDRAULIC SERVOVALVES
    MIL-P-8564 Revision D:1970 PNEUMATIC SYSTEM COMPONENTS, AERONAUTICAL, GENERAL SPECIFICATION FOR [ASG]
    ASME Y14.100 : 2017 ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES
    IEEE 12207.2-1997 IEEE/EIA Guide - Industry Implementation of International Standard ISO/IEC 12207 : 1995 (ISO/IEC 12207) Standard for Information Technology- Software Life Cycle Processes - Implementation considerations
    MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
    FAA AC 121.195-1 : 0 OPERATIONAL LANDING DISTANCES FOR WET RUNWAYS; TRANSPORT CATEGORY AIRPLANES
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