SAE ARP5412B
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
Hardcopy , PDF
17-10-2024
English
11-01-2013
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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 |
Superseded
|
| SupersededBy | |
| 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 ARP5414A | 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 ARP5415A | 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 ARP5414A | AIRCRAFT LIGHTNING ZONE |
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