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"Kevin Horton" wrote in message (1) Some composites are susceptible to
lightning damage, and do not dissipate Pstatic electrical charges or provide electromagnetic shielding. Therefore it should be demonstrated by analysis support by test evidence that the structure can dissipate P-static electrical charges, provides electromagnetic protection where required and provides an acceptable means of diverting the resulting electrical current (as a result of a lightning strike) so as not to endanger the aircraft. (2) Consideration should be given possible deterioration and undetected damage to the lightning protection system. That spells out the requirements. Other than the thin copper mesh already mentioned, how are manufacturers meeting these requirements? D. |
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