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基本信息

【范围】

This user's manual provides additional information and references relevant to identifying: (1) acceptance criteria for the indirect effects of lightning compliance approaches, (2) verification (analysis and test) methods including those associated with multiple stroke and multiple burst and (3) recommended design options to optimize needed system immunity to lightning indirect effects. Equipment hazards addressed include those due to the indirect effects on equipment mounted on the aircraft exterior and equipment located within the aircraft interior as well as all associated interconnecting wiring. This document has specific application toward those topics and subsystems addressed in ARP5413 but also provides additional guidelines in the application of those tests identified in DO-160/ED-14, Section 22. 1.1 Purpose: This user's manual expands on the topics introduced in ARP5413, Certification of Aircraft Electrical/ Electronic Systems for the Indirect Effects of Lightning. Guidelines are provided which explain the approaches to compliance with the US Federal Aviation Regulations (FAR) and the European Joint Airworthiness Regulations (JAR). Discussions are applicable to all categories of airplanes and rotorcraft. This material as well as the Aerospace Recommended Practices (ARPs) it supports are not intended to provide mandatory approaches to compliance. In many cases, the path to compliance may use one or more of several methods. Applicants for Federal Aviation Administration (FAA) or Joint Aviation Authority (JAA) approval may elect to demonstrate compliance through alternative methods found acceptable by the FAA/JAA.strRefField

【与前一版的变化】

包含缩略语

A：
AC：
C：
cm：
dB：
DC：
f or F：
I：
K：
kA：
kHz：
L：
mA：
MHz：
μH：
μs：
mm：
nH：
P：
ps：
Q：
R：
V：
W：
Z：
AC：
AFWL：
ARINC：
ARP：
ATL：
ATS：
AWG：
BITE：
CFC：
CMOS：
CMR：
CW：
DAL：
DAU：
DOT：
EDAC：
EFIS：
EICAS：
EME：
EMI：
EMP：
ETDL：
ETSL：
EUROCAE：
EUT：
FAA：
FADEC：
FAR：
FBW：
FCC：
FHA：
FWD：
GUI：
HIRF：
HP Bleed：
IFR：
IR：
JAA：
JAR：
LLPT：
LLSC：
LP Bleed：
LRU：
LTA：
LVDT：
MB：
MIL-HDBK：
MIL-STD：
MOSFET：
MOV：
MS：
MTBF：
MTBUR：
NASA：
NIST：
NTIS：
OAS：
PAT：
PMA：
PRF：
RF：
RTCA：
SAE：
SCEPTRE：
SPD：
SPICE：
STC：
TC：
TCL：
TDFD：
TPD：
TR：
TSO：
USAF：
VFR：
WG：

替代标准

ARP5415

引用文件/被引文件

AC 20-53A

"Protection of Aircraft Fuel Systems Against Fuel Vapor Ignition Due to Lightning”. AC 20-53A contains zoning definitions and procedures that are used for direct effects protection and is used as a guide to describe zoning as it applies to indirect effects.

AC 23.1309-1C

"System Design and Analysis"

AC 25.1309-1A

“System Design and Analysis"

AC 27-1A

“Certification of Normal Category Rotorcraft”

AC 29-2B

“Certification of Transport Category Rotorcraft”

DOT/FAA/CT-89/22

"Aircraft Lightning Protection Handbook"

MIL-HDBK-217F

"Military Handbook

MIL-STD-461E

"Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment"

MIL-STD-464

“Electromagnetic Environmental Effects Requirements for Systems”

MIL-STD-882D

"Standard Practice for System Safety"

D180-27423-49

“Atmospheric Electricity Hazards Protection

ARP4754

“Certification Considerations for Highly Integrated or Complex Aircraft Systems”

ARP4761

“Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipment”

ARP5412

"Aircraft Lightning Environment and Related Test Waveforms"

ARP5413

"Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning"

ARP5414

"Aircraft Lightning Zoning"

ARP5416

“Aircraft Lightning Test Methods” – (Draft)

RTCA/DO-160D

"Environmental Conditions and Test Procedures for Airborne Equipment"

RTCA/DO-178B

"Software Considerations in Airborne Systems and Equipment Certification"

EUROCAE ED-14

"Environmental Conditions and Test Procedures for Airborne Equipment"

EUROCAE ED-84

"Aircraft Lightning Environment and Related Test Waveforms Standard"

相关标准

·AIR1047D

A Guide for the Selection of Quick-Disconnect Couplings for Aerospace Fluid Systems

·AIR1075A

BAROMETRY FOR ALTIMETER CALIBRATION

·AIR1087B

Aircraft Accessory Drag Torque During Engine Starts

·AIR1093A

Numeral, Letter and Symbol Dimensions for Aircraft Instrument Displays

·AIR1106A

Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights

·AIR1147A

Electromagnetic Interference on Aircraft From Jet Engine Charging

·AIR1169B

Bibliography of References Pertaining to The Effects of Oxygen on Ignition and Combustion of Materials

·AIR1174B

Index of Starting System Specifications and Standards

·AIR1191A

Performance of Low Pressure Ratio Ejectors for Engine Nacelle Cooling

·AIR1204A

(R) Control of Water Carryover from the Environmental Control System and Condensation on the Structure

包含图表

Nomenclature Cross R	Zonal Application of	formula 1
formula 2	formula 3	formula 4
formula 5	formula 6	formula 7
formula 8	TCL and ETDL Selecti	Waveform Set Selecti
Simple System Expose	formula 9	Typical Pin Injectio
Equipment Pins With	Equipment Pins With	Equipment Pins With
Typical Wire Bundle	Typical Ground Injec	Swept Frequency Test
formula 10	Low Current Pulse Te	High Current Pulse T
Common Test Entry/Ex	Schematic Representa	Examples of Similari
Bulk Wire Bundle Cur	Attenuation Provided	Attenuation Due to A
Single Shielded Wire	Single Shielded Wire	Single Shielded Wire
Single Unshielded Wi	Single Unshielded Wi	Single Unshielded Wi
Example Avionics Ins	Summary of Current L	FADEC System Block D
Fire Wall Penetratio	Fire Wall Penetratio	Fire Wall Penetratio
Effective Cross Sect	formula 11	FADEC Initial Strike
Summary for Level A	Example Avionics Ins	Applicable Maintenan
Aircraft Structure S	Wiring Installation	Analysis and Test Pr
Aperture Coupled Fie	Field Topology Effec	Wire and Circuit Cou
Wire in a Conductive	Structure Section	formula 12
formula 13	Fundamental Transmis	formula 14
formula 15	formula 16	formula 17
Natural Response Ene	Total Response Energ	Forced Response (Onl
formula 18	Transfer Function -	formula 19
formula 20	formula 21	formula 22
formula 23	formula 24	formula 25
formula 26	formula 27	formula 28
formula 29	Early Time Response	Early Time Response
Time History of Inte	Time History of Elec	Time History of Elec
formula 30	formula 31	Transfer Function -
Wing Box Analyzed Wi	Setup for Tests on W	Locations Where Volt
Locatioins Where Cur	Low and High Level T	Time and Space Resol
Comparison of Analyt	Comparison of Analyt	Comparison of Wavesh
Single Point Circuit	Multiple Point Circu	Shield Terminations
Daisy Chain Terminat