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SAE ARP 5416 : 2013

Current
Current

The latest, up-to-date edition.

AIRCRAFT LIGHTNING TEST METHODS
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-07-2013

Publisher

SAE International

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

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

Committee
AE-2
DocumentType
Revision
Pages
105
PublisherName
SAE International
Status
Current
Supersedes

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

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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