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  • SAE ARP 5416 : 2013

    Current The latest, up-to-date edition.

    AIRCRAFT LIGHTNING TEST METHODS

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  07-01-2013

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. LIGHTNING EFFECTS
    4. PLANNING OF LIGHTNING EFFECTS TESTS
    5. DIRECT EFFECTS TEST METHODS
    6. INDIRECT EFFECTS TEST METHODS
    7. FUEL SYSTEM TEST METHODS
    8. TEST REPORT
    9. NOTES

    Abstract - (Show below) - (Hide below)

    Provides test techniques for simulated lightning testing of aircraft and the associated systems.

    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
    SAE ARP 5412 : 2013 AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
    SAE ARP 5414 : 2012 AIRCRAFT LIGHTNING ZONE
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    SAE AS 5830 : 2017 COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF-BONDING, PROCUREMENT SPECIFICATION
    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 AIR 6464 : 2013 EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES
    SAE AS 7510 : 2017 COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION
    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
    AECTP-250 : 2014 ELECTRICAL AND ELECTROMAGNETIC ENVIRONMENTAL CONDITIONS
    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
    SAE AS 6116 : 2016 ALUMINUM FITTINGS, AXIALLY SWAGED TUBE WITH FLARELESS SEPERABLE, FLUID SYSTEM, UP TO 1500 PSI (10340 KPA) MAXIMUM, SPECIFICATION FOR

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

    FAA AC 27-1 : 2008 CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
    IEC 60060-2:2010 High-voltage test techniques - Part 2: Measuring systems
    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 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    SAE ARP 5415 : 2002 USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING
    ANSI/NCSL Z540 1 : 94(R2002) CALIBRATION - CALIBRATION LABORATORIES AND MEASURING AND TEST EQUIPMENT - GENERAL REQUIREMENTS
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    SAE ARP 5414 : 2012 AIRCRAFT LIGHTNING ZONE
    SAE ARP 5412 : 2013 AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
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