THE CERTIFICATION OF AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEMS FOR OPERATION IN THE HIGH-INTENSITY RADIATED FIELDS (HIRF) ENVIRONMENT

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2014

Publisher

Federal Aviation Administration

1. Purpose
2. Applicability
3. Related Material
4. Background
5. Definitions
6. Approaches to Compliance
7. Margins
8. HIRF Compliance
9. Steps to Level A System HIRF Compliance
10. Steps to Level B and C System HIRF Compliance
11. Maintenance, Protection Assurance, and Modifications
Appendix 1 - Generic Transfer Functions and Attenuation
Appendix 2 - Advisory Circular Feedback Information

Helps you with information and guidance on how to show compliance with Title 14, Code of Federal Regulations (14 CFR) 23.1308, 25.1317, 27.1317, and 29.1317, High-intensity Radiated Fields (HIRF) Protection.

DocumentType	Standard
Pages	38
PublisherName	Federal Aviation Administration
Status	Current

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 20-184 : 2015	GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
SAE AIR 4004 : 2015	GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR
SAE ARP 60493 : 2017	GUIDE TO CIVIL AIRCRAFT ELECTROMAGNETIC COMPATIBILITY (EMC)
FAA AC 20-180 : 2013	APPROVED MODEL LIST SUPPLEMENTAL TYPE CERTIFICATE (AML-STC)
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 121-22 : 2012	MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES
SAE AS 8055A : 2015	MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD)
SAE AIR 5924 : 2013	GUIDELINES FOR THE INTEGRATION OF ELECTRONIC ENGINE CONTROL SYSTEMS FOR TRANSPORT CATEGORY (PART 25) AND GENERAL AVIATION (PART 23) AIRCRAFT
SAE AS 5498 : 2017	MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR INFLIGHT ICING DETECTION SYSTEMS
FAA AC 23.1309-1 : 2011	SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
SAE ARP 5794 : 2014	CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD

FAA AC 27-1 : 2008	CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT
SAE ARP 4754 : 2010	GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
SAE ARP 4761 : 1996	GUIDELINES AND METHODS FOR CONDUCTION 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 ARP 5583 : 2010	GUIDE TO CERTIFICATION OF AIRCRAFT IN A HIGH-INTENSITY RADIATED FIELD (HIRF) ENVIRONMENT
FAA AC 29-2 : 2008	CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
FAA AC 25.1309-1 : 0	SYSTEM DESIGN AND ANALYSIS

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FAA AC 20-158 : 2014

Current

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