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  • SAE ARP 5412 : 2013

    Current The latest, up-to-date edition.

    AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  11-01-2013

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. BACKGROUND
    4. NATURAL LIGHTNING DESCRIPTION
    5. LIGHTNING INTERACTIONS WITH AIRCRAFT
    6. IDEALIZED STANDARD EXTERNAL LIGHTNING ENVIRONMENT
    7. IDEALIZED STANDARD INDUCED TRANSIENT WAVEFORMS
    8. SUMMARY OF WAVEFORMS/WAVEFORM SETS
    9. NOTES
    APPENDIX A - MEASURED LIGHTNING PARAMETER DATA

    Abstract - (Show below) - (Hide below)

    The environment and test waveforms defined in this SAE Aerospace Recommended Practice (ARP) account for the best lightning data and analysis currently available.

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

    Committee AE-2
    Document Type Revision
    Publisher SAE International
    Status Current
    Supersedes

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

    FAA AC 20-155 : 2013 INDUSTRY DOCUMENTS TO SUPPORT AIRCRAFT LIGHTNING PROTECTION CERTIFICATION
    BS ISO 14302:2002 Aerospace series. Space systems. Electromagnetic compatibility requirements
    SAE AS 6116 : 2016 ALUMINUM FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPERABLE, FLUID SYSTEM, UP TO 1500 PSI (10340 KPA) MAXIMUM, SPECIFICATION FOR
    SAE ARP 5416 : 2013 AIRCRAFT LIGHTNING TEST METHODS
    SAE ARP 5414 : 2012 AIRCRAFT LIGHTNING ZONE
    SAE AIR 6464 : 2013 EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    FAA AC 25-11 : 2014 ELECTRONIC FLIGHT DISPLAYS
    SAE AIR5691A : 2017 GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS
    SAE AS 5958 : 2017 FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPARABLE, FLUID SYSTEM FOR OPERATING PRESSURES UP TO AND INCLUDING 5080 PSI (35 000 KPA), SPECIFICATION FOR
    S.R. CWA 17044:2016 AEROSPACE SERIES - MODULES FOR ELECTRO-MECHANICAL ACTUATORS IN AIRCRAFT
    NASA STD 4003 : 2013 ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT
    SAE AS 5830 : 2017 COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF-BONDING, PROCUREMENT SPECIFICATION
    MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
    MIL-STD-464 Revision C:2010 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
    14/30310862 DC : 0 BS EN 4832 - AEROSPACE SERIES - ADAPTOR, PIPE COUPLING 24 DEGREES CONE UP TO 35000 KPA (5080 PSI) RING-LOCKED FITTING AND RING-LOCKED FITTING-REDUCER - INCH SERIES - TECHNICAL SPECIFICATION
    SAE AIR 6185 : 2015 AEROSPACE - LIGHTNING EFFECTS ON HYDRAULIC TRANSPORT ELEMENTS ON AIRCRAFT
    SAE AIR 5774 : 2012 COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS
    SAE AS 7510 : 2017 COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION
    NASA JSC 08080-2 : 2015 JSC DESIGN AND PROCEDURAL STANDARDS
    AEP-41 VOL 1 : 2004 UNIFIED ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) PROTECTION, PHILOSOPHY AND METHODOLOGY
    SAE AIR1184B : 2016 CAPACITIVE FUEL GAUGING SYSTEM ACCURACIES
    SAE AS 5000 : 2010 FITTING, PLUG-IN UNION, RING LOCKED, 24 DEGREE CONE, FLUID CONNECTION, 5080 PSI (35000 KPA), SPECIFICATION FOR
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    ISO 14302:2002 Space systems Electromagnetic compatibility requirements
    09/30190333 DC : 0 BS EN 61400-24 - WIND TURBINES - PART 24: LIGHTNING PROTECTION
    API 545 : 2009 RECOMMENDED PRACTICE FOR LIGHTNING PROTECTION OF ABOVEGROUND STORAGE TANKS FOR FLAMMABLE OR COMBUSTIBLE LIQUIDS
    SAE ARP 5415 : 2008 USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING
    SAE AIR 4004 : 2015 GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR

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

    FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
    FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
    FAA AC 20-53 : 2006 PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    SAE ARP 5415 : 2002 USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    SAE ARP 5416 : 2013 AIRCRAFT LIGHTNING TEST METHODS
    FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
    FAA AC 20-155 : 2013 INDUSTRY DOCUMENTS TO SUPPORT AIRCRAFT LIGHTNING PROTECTION CERTIFICATION
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    SAE ARP 5414 : 2012 AIRCRAFT LIGHTNING ZONE
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