FAA AC 20-184 : 2015
Current
The latest, up-to-date edition.
GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
Hardcopy , PDF
English
01-01-2015
CHAPTER 1 - Introduction
CHAPTER 2 - Installation of Lithium Batteries on Aircraft
CHAPTER 3 - Maintenance and Operational Considerations
for Lithium Battery Systems
Appendix A - Definition of Size in Terms of Watt Hours (Wh)
on Lithium Battery and Battery Systems
Appendix B - Related Regulations and Documents
Appendix C - Terms and Definitions
Appendix D - Typical Special Condition (SC) and Intent for Each
SC for Parts 23, 25, 27, and 29D-1
Appendix E - MOC for Small and Medium Lithium Batteries
(Using RTCA DO-347 MOPs)
Appendix F - MOC for Large Lithium Batteries and Battery Systems
(Using RTCA DO-311 and Some Tests of DO-347 MOPs)
Appendix G - Flow Chart for Lithium battery Means of Compliance
certification Process
Appendix H - Advisory Circular Feedback Information
Gives an acceptable means to show compliance to the airworthiness requirements for installed rechargeable lithium battery and battery systems on aircraft using standards provided in RTCA, Inc., documents RTCA DO-347 and RTCA DO-311.
DocumentType |
Standard
|
Pages |
41
|
PublisherName |
Federal Aviation Administration
|
Status |
Current
|
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FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
FAA AC 43.13-2 : 2008 | ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT ALTERATIONS |
FAA AC 21-16 : 2011 | RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT" |
RTCA DO 347 : 2013 | CERTIFICATION TEST GUIDANCE FOR SMALL AND MEDIUM SIZED RECHARGEABLE LITHIUM BATTERIES AND BATTERY SYSTEMS |
RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
FAA 8110.4 : 2011 | TYPE CERTIFICATION |
SAE ARP 4754 : 2010 | GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS |
FAA AC 20-158 : 2014 | THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT |
FAA AC 25-16 : 0 | ELECTRICAL FAULT AND FIRE PREVENTION AND PROTECTION |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
FAA AC 20-152 : 2005 | RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE ARP 4761 : 1996 | GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
FAA 8110.42 : 2014 | PARTS MANUFACTURER APPROVAL PROCEDURES |
FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
FAA AC 120-16 : 2016 | AIR CARRIER MAINTENANCE PROGRAMS |
FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
FAA AC 25.1581-1 : 2012 | AIRPLANE FLIGHT MANUAL |
FAA AC 23-17 : 2011 | SYSTEMS AND EQUIPMENT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
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FAA AC 120-42 : 2008 | EXTENDED OPERATIONS (ETOPS AND POLAR OPERATIONS) |
FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
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