EUROCAE ED 81
CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTING
| Organization: | EUROCAE |
| Publication Date: | 1 May 1996 |
| Status: | active |
| Page Count: | 34 |
scope:
This report provides guidance for a means of showing compliance
with the regulations for hazards caused by the lightning
environment to electrical/electroni
NOTE:
This report 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 Section 4 of this document). This report does not address lightning zoning methods or lightning test requirements, methods, and techniques. Coverings (fairing, skin, cowl, etc.) should normally prevent 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 evolution of both direct and indirect effects will be necessary.
It should be noted that electrical/electroni
PURPOSE
This report provides information and guidance concerning a
means, but not the only means, of compliance with Parts 12, 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/electroni
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