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SAE ARP 5412 : 2013

Current
Current

The latest, up-to-date edition.

AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-11-2013

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

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

Committee
AE-2
DocumentType
Revision
Pages
63
PublisherName
SAE International
Status
Current
Supersedes

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

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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