SAE ARP 5416 : 2013
Current
The latest, up-to-date edition.
AIRCRAFT LIGHTNING TEST METHODS
Hardcopy , PDF
English
07-01-2013
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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