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Protection of electrical and electronic equipment against lightning indirect effects on the Airbus A340 wingThe provisions applied to the Airbus A340 wing wiring against lightning indirect effects are presented. The construction and installation of the wiring's shielding systems are described, and the analysis and tests performed to determine the effectiveness of the measures taken are discussed. A first evaluation of the results of the theoretical analysis together with the provisional results of tests indicate a sufficient safety margin between required and achieved protection levels.
Document ID
19910023299
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Spiller, Olaf (Deutsche Airbus G.m.b.H. Bremen, Germany)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Publication Information
Publication: NASA. Kennedy Space Center, The 1991 International Aerospace and Ground Conference on Lightning and Static Electricity, Volume 1
Subject Category
Air Transportation And Safety
Accession Number
91N32613
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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