SAE ARP 5414 : 2012

Superseded

View Superseded by

AIRCRAFT LIGHTNING ZONE

Available format(s)

Hardcopy , PDF

Superseded date

10-12-2018

Language(s)

English

Published date

01-01-2012

Publisher

SAE International

1 SCOPE
2 REFERENCES
3 BACKGROUND
4 AIRCRAFT LIGHTNING INTERACTION
5 ZONE DEFINITIONS
6 WAVEFORM APPLICABILITY
7 ZONE LOCATION PROCESS
8 INITIAL LEADER ATTACHMENT LOCATION METHODS
9 OTHER ZONING CONSIDERATIONS
10 PROTECTION CONSIDERATIONS
11 NOTES

Defines lightning strike zones and provides guidelines for locating them on particular aircraft, together with examples.

Committee	AE-2
DocumentType	Standard
Pages	33
PublisherName	SAE International
Status	Superseded
SupersededBy	SAE ARP5414B:2018
Supersedes	SAE ARP 5414 : 2005

FAA AC 20-155 : 2013	INDUSTRY DOCUMENTS TO SUPPORT AIRCRAFT LIGHTNING PROTECTION CERTIFICATION
SAE ARP 5412 : 2013	AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
MIL-STD-461 Revision G:2015	REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
SAE AIR5691A : 2017	GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS
FAA AC 25-11 : 2014	ELECTRONIC FLIGHT DISPLAYS
NASA STD 4003 : 2013	ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT
MIL-STD-464 Revision C:2010	ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
SAE AIR 6185 : 2015	AEROSPACE - LIGHTNING EFFECTS ON HYDRAULIC TRANSPORT ELEMENTS ON AIRCRAFT
SAE ARP 5416 : 2013	AIRCRAFT LIGHTNING TEST METHODS
SAE AS 8017 : 2017	MINIMUM PERFORMANCE STANDARD FOR ANTICOLLISION LIGHT SYSTEMS
NASA JSC 08080-2 : 2015	JSC DESIGN AND PROCEDURAL STANDARDS
SAE AIR 6464 : 2013	EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES
FAA AC 20-136 : 2011	AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
SAE AIR 5774 : 2012	COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS
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

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
SAE ARP 5412 : 2013	AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS

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SAE ARP 5414 : 2012

Superseded

Table of Contents

Abstract

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Standards Referenced By This Book

Standards Referencing This Book

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