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SAE ARP5413
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SAE ARP5413 Revision A, March 1, 2007
Certification of Aircraft Electrical/Electronic Systems for the Indirect
Effects of Lightning
Description / Abstract:
This SAE Aerospace Recommended Practice (ARP) provides guidance
for a means of showing compliance with the regulations for hazards
caused by the lightning environment to electrical/ electronic
systems installed either on or within aircraft. Equipment hazards
addressed include those due to indirect effects on equipment and
its associated wiring that is mounted on the aircraft exterior as
well as indirect effects on equipment and its associated wiring
located within the aircraft interior. This document applies to new
aircraft and equipment designs, modifications of existing aircraft
or equipment, and applications of existing (off the shelf)
equipment on new aircraft.
NOTE: This ARP does not address direct effects such as burning, eroding, blasting, of aircraft structure nor does it address fuel ignition hazards (see related reading material in 2.3 of this document). This ARP does not address lightning zoning methods or lightning test requirements, methods, and techniques. Coverings (fairing, skin, cowl, etc.) should normally prevent direct attachment of the lightning channel to underlying system components. However, if a direct lightning strike attachment to a system component can occur, a complete evaluation of both direct and indirect effects will be necessary.
It should be noted that electrical/electronic systems or components are sometimes exposed to lightning currents directly conducted from the aircraft exterior, as may happen when an antenna is struck and a portion of lightning current flows in its cable. Care should be taken to identify any such possibilities and either eliminate these situations by design modifications, or address them in the certification plan. No further discussion of these situations is included in this ARP.
Purpose:
This ARP provides information and guidance concerning a means, but not the only means, of compliance with Parts 23, 25, 27, and 29 of the Federal Aviation Regulations (FAR) and Joint Airworthiness Requirements (JAR), as applicable for preventing hazards, due to lightning indirect effects, from occurring to electrical/electronic systems.
NOTE: This ARP does not address direct effects such as burning, eroding, blasting, of aircraft structure nor does it address fuel ignition hazards (see related reading material in 2.3 of this document). This ARP does not address lightning zoning methods or lightning test requirements, methods, and techniques. Coverings (fairing, skin, cowl, etc.) should normally prevent direct attachment of the lightning channel to underlying system components. However, if a direct lightning strike attachment to a system component can occur, a complete evaluation of both direct and indirect effects will be necessary.
It should be noted that electrical/electronic systems or components are sometimes exposed to lightning currents directly conducted from the aircraft exterior, as may happen when an antenna is struck and a portion of lightning current flows in its cable. Care should be taken to identify any such possibilities and either eliminate these situations by design modifications, or address them in the certification plan. No further discussion of these situations is included in this ARP.
Purpose:
This ARP provides information and guidance concerning a means, but not the only means, of compliance with Parts 23, 25, 27, and 29 of the Federal Aviation Regulations (FAR) and Joint Airworthiness Requirements (JAR), as applicable for preventing hazards, due to lightning indirect effects, from occurring to electrical/electronic systems.
SAE ARP5413 Revision A, March 1, 2007
Certification of Aircraft Electrical/Electronic Systems for the Indirect
Effects of Lightning