FAA AC 20-136 : 2011
Current
Current
The latest, up-to-date edition.
AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
01-01-2011
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. Purpose
2. Applicability
3. Scope
4. Cancellation
5. Background
6. Steps for Showing Compliance
7. Effects of Transients
8. Level A System Lightning Certification
9. Level B and C System Lightning Certification
10. Maintenance and Surveillance
Appendix 1 - Related Documents and How to Get Them
Appendix 2 - Definitions
Appendix 3 - Acronyms
Gives you information and guidance on how you can protect aircraft electrical and electronic systems from the effects of lightning.
| DocumentType |
Standard
|
| Pages |
27
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
| FAA AC 23-15 : 2003 | SMALL AIRPLANE CERTIFICATION COMPLIANCE PROGRAM |
| FAA AC 20-170 : 2013 | INTEGRATED MODULAR AVIONICS DEVELOPMENT, VERIFICATION, INTEGRATION, AND APPROVAL USING RTCA/DO-297 AND TECHNICAL STANDARD ORDER-C153 |
| FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
| FAA AC 33.4-3 : 2005 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS; AIRCRAFT ENGINE HIGH INTENSITY RADIATED FIELDS (HIRF) AND LIGHTNING PROTECTION FEATURES |
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
| FAA AC 20-184 : 2015 | GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT |
| FAA AC 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
| SAE AS8054A | Airborne Engine Vibration Monitoring (EVM) System, Guidelines for Performance Standard For |
| FAA AC 20-180 : 2013 | APPROVED MODEL LIST SUPPLEMENTAL TYPE CERTIFICATE (AML-STC) |
| SAE ARP5414A | Aircraft Lightning Zone |
| FAA AC 25.899-1 : 2007 | ELECTRICAL BONDING AND PROTECTION AGAINST STATIC ELECTRICITY |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| SAE ARP5794 | Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard |
| FAA AC 20-177 : 2012 | DESIGN AND INSTALLATION GUIDANCE FOR AN AIRBORNE SYSTEM FOR NON-REQUIRED TELECOMMUNICATION SERVICE IN NON-AERONAUTICAL FREQUENCY BANDS |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| SAE AIR 6464 : 2013 | EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES |
| FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
| SAE AIR6185 | Aerospace - Lightning Effects on Hydraulic Transport Elements on Aircraft |
| SAE ARP5416A | Aircraft Lightning Test Methods |
| FAA AC 121-22 : 2012 | MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES |
| NASA JSC 08080-2 : 2015 | JSC DESIGN AND PROCEDURAL STANDARDS |
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
| FAA AC 20-156 : 2006 | AVIATION DATABUS ASSURANCE |
| SAE AS8055A | Minimum Performance Standard for Airborne Head Up Display (HUD) |
| SAE AIR5924A | Guidelines for the Integration of Electronic Engine Control Systems for Transport Category (Part 25) and General Aviation (Part 23) Aircraft |
| SAE AIR 4567 : 2014 | COMPOSITE ELECTRICAL CONNECTORS |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
| FAA AC 20-149 : 2015 | INSTALLATION GUIDANCE FOR DOMESTIC FLIGHT INFORMATION SERVICE - BROADCAST |
| 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" |
| SAE ARP4754A | 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 |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| SAE ARP5416A | Aircraft Lightning Test Methods |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| FAA AC 23-17 : 2011 | SYSTEMS AND EQUIPMENT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| FAA AC 20-155 : 2013 | INDUSTRY DOCUMENTS TO SUPPORT AIRCRAFT LIGHTNING PROTECTION CERTIFICATION |
| SAE ARP 5577 : 2002 | AIRCRAFT LIGHTNING DIRECT EFFECTS CERTIFICATION |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| SAE ARP5414A | Aircraft Lightning Zone |
| SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
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