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Environmental Conditions and Test Procedures for Airborne Equipment

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发表于 2021-11-5 14:45:51 | 显示全部楼层 |阅读模式
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RTCA DO-160E Environmental Conditions and TestProcedures for Airborne Equipment 航空电子设备的电磁兼容要求. 这个不是最新版本,最新版本是RTCA DO-160G.

ForewordThis document was prepared by Special Committee 135 (SC-135) and approved by the RTCAProgram Management Committee (PMC) on December 9, 2004. It supersedes RTCA DO-160Ddated July 29, 1997; Change 1 dated December 14, 2000; Change 2 dated June 21, 2001; andChange 3 dated December 5, 2002.RTCA, Incorporated is a not-for-profit corporation formed to advance the art and science ofaviation and aviation electronic systems for the benefit of the public. The organization functionsas a Federal AdvISOry Committee and develops consensus based recommendations oncontemporary aviation issues. RTCA’s objectives include but are not limited to:• coalescing aviation system user and provider technical requirements in a manner thathelps government and industry meet their mutual objectives and responsibilities;• analyzing and recommending solutions to the system technical issues that aviation facesas it continues to pursue increased safety, system capacity and efficiency;• developing consensus on the application of pertinent technology to fulfill user andprovider requirements, including development of minimum operational performancestandards for electronic systems and equipment that support aviation; and• assisting in developing the appropriate technical material upon which positions for theInternational Civil Aviation Organization and the International TelecommunicationsUnion and other appropriate international organizations can be based.The organization’s recommendations are often used as the basis for government and privatesector decisions as well as the foundation for many Federal Aviation Administration technicalStandard Orders.Since RTCA is not an official agency of the United States Government, its recommendations maynot be regarded as statements of official government policy unless so enunciated by the U.S.government organization or agency having statutory jurisdiction over any matters to which therecommendations relate.These standards were coordinated by RTCA SC-135 with the European Organisation for CivilAviation Equipment (EUROCAE) Working Groups (WGs) 14 and 31. EUROCAE concurs withRTCA on the environmental conditions and test procedures set forth herein. When approved byEUROCAE, this document will be identified jointly as RTCA DO-160E/EUROCAE ED-14E.


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