Rtca do 160f pdf
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the document includes 26 sections and three appendices. rtca has teamed with wichita state university’ s national institute for aviation research ( wsu- niar) to offer high quality training covering rtca’ s do- 160g, environmental conditions and test procedures for airborne equipment. minimum operational performance standards for airborne radio communications equipment operating within the radio frequency range 117. do- 160d, “ environmental conditions and test procedures for airborne equipment, ” dated j, and discusses how the document may be used in showing compliance with airworthiness requirements. the information in the table will assist you in determining if a particular version of rtca/ do- 160 is acceptable. foreword this report was prepared by rtca special committee 135 ( sc- 135) and approved by the rtca program management committee ( pmc) on decem. minimum operational performance standards for airborne radio communications equipment operating within the radio 1995 frequency range 117. environmental conditions and test procedures for airborne equipment. rtca do- 160 section 6 – humidity. rtca/ do- 160e is also acceptable to meet the hirf requirements for level b and c systems when using test levels defined in the appropriate regulations as discussed in ac 20- 158. it is published by the radio rtca do 160f pdf technical commission for aeronautics ( rtca) and supersedes do- 138. available in hardcopy* * * do- 186a. for additional guidance on hirf, refer to the latest revision of ac 20- 158. 1317, use rtca/ do- 160f or g. this page intentionally left blank. 1 140connecticut avenue, n w suite 1020 washington, dc 6 telephone: rtcndo- 160d environmental conditions andtest procedures for airborne equipment s f! cookie information is stored in your browser and performs functions such as recognising you when you return to our website and helping our team to understand which sections of the website you find most interesting and useful. this website uses cookies so that we can provide you with the best user experience possible. this document was prepared by special committee 135 ( sc- 135) and was approved by the rtca program management committee ( pmc) on decem. the purpose of do- 160 humidity testing is to assess the ability of airborne equipment to endure exposure to natural or induced humidity, which can cause corrosion, altering of metals, conductors and insulators, and changes to the chemical properties of equipment. these standards were coordinated by rtca sc- 1 35 with the european organisation for civil aviation equipment ( eurocae). when approved by eurocae, this document will be identified jointly as rtca do- 160f/ eurocae ed- 14f. 1( a) change from: maintain surfaces in a wetted condition for 8 hours followed by a drying period of 16 hours at 65° c. rtca do- 160g provides standard procedures and environmental test criteria for testing airborne equipment for the entire spectrum of aircraft from light general aviation aircraft and helicopters through the “ jumbo jets” and sst categories of aircraft. the current version is do- 160g, published in and is referenced for use by faa’ s advisory circular ac 21- 16g as well. rtca/ do- 160g and its european twin, eurocae/ ed- 14g, are identically worded. document history. review of the i· r- voltage drop in composite- skinned systems, coupling to cables, copper. do- 160, environmental conditions and test procedures for airborne equipment is a standard for the environmental testing of avionics hardware. this advisory circular calls attention to rtca, inc ( formerly radio technical commission for aeronautics) document no. the faa strongly encourages the use of rtca/ do- 160g for new articles. ac 21- 16g ( pdf). this note addresses specific test methods in do- 160f however, in order to develop the rationale, we will treat system level pdf effects first followed by coupling to cables and then to wires and pins. many of these changes stem from changes in construction materials used in the fabrication of airplanes. the designation do stands for " document". rtca, incorporated is a not- for- profit. the course will provide an understanding of the use of do- 160g and how it fits in with the greater. appendix 1 of this ac provides a summary of the changes from rtca/ do- 160c to rtca/ do- 160d, version d to e, version e to f, and f to g. eurocae concurs with rtca on the environmental conditions and test procedures set forth herein. rtca, incorporated is a not- for- profit corporation formed to advance the art and science of aviation and aviation electronic systems for the benefit of the public. a list of standards published by rtca, incorporated. as many in the aerospace test industry are aware, there have been many changes to, and revisions of, do- 160, section 22, within the past few years. rtca / do- 160 section 6 includes three. it is required to rtca do 160f pdf specify fluids used, test method and temperature of exposure in the test procedure and the environmental qualification form. try our free test plan generator. finally, pdf we will look at the future direction of sc- 135, and the timetable. the original do- 160 standard was published in 1975 to provide standard test methods which would ensure new aviation equipment would function appropriately in the multiple environmental and emi conditions found on aircraft. salt spray important notice information pertinentto this test procedure is contained in sections 1, 2 and 3. fundamentals of rtca/ do- 160f, section 22: lightning induced transient susceptibility. in contrast, do- 160f starts with pin injection tests. changes in each section since the release of do- 160f will be summarized. the purpose of this article is to provide an overview of each of the sections that deal with emc in do- 160g. do- 220 chg 1 do- 227 do- 228 rtca rtca.