Rtca do 160g pdf

Rtca do 160g pdf

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the purpose of this article is to provide an overview of each of the sections that deal with emc in do- 160g. supplement to do- 160g. 1 140 connecticut avenue, nw, suite 1020 washington, dcusa telephone:. download rtca do- 160g free in pdf format. do- 160 is the standard that defines environmental test conditions and applicable test procedures and criteria for avionic equipment. published 5 aprile at pdf 700 × 125 in lightning induced transient susceptibility. rtca, incorporated 1140 connecticut avenue, n. the tests in rtca/ do- 160 provide a laboratory means of demonstrating the performance characteristics of airborne. do- 160g – electronic. these standards were coordinated by rtca sc - 135 with the european organisation for civil aviation e quipment ( eurocae). the information in the table will assist you in determining if a particular version of rtca/ do- 160 is acceptable. the current version rtca do 160g pdf is do- 160g, published in and is referenced for use by faa’ s advisory circular ac 21- 16g as well. they create lightning through the heart of the cloud). it defines standard environmental test conditions ( categories) and applicable test procedures for airborne equipment. there are three ( 3) types of lightning flashes which may occur:. rtca/ do- 160g and its european twin, eurocae/ ed- 14g, are identically worded. 1( a) change from: maintain surfaces in a wetted condition for 8 hours followed by a drying period of 16 hours at 65° c. the focus of this group is the procedure for flammability testing electronic equipment installed on aircraft. lightning flashes are the discharging of strong electric fields, or charge centers, within cumulonimbus clouds ( cumulonimbus clouds can form alone, in clusters, or along a cold front in a squall line. rtca/ do- 160d, version d to e, version e to f, and f to g. download rtca- do- 160d. cable induction is a method used to apply any of the do- 160g specified waveforms onto the interconnecting wires rtca do 160g pdf or cable bundles. subscribe to our newsletter. note: when reference to rtca/ do- 160d is made in this ac, it includes changes 1, 2, and 3, dated decem, j, and decem, respectively. rtca do- 357 prepared by: sc- 135. welcome to dlscrib. 1150 18th street, nw, suite 910. conditions and procedures in a different version of rtca/ do- 160 instead of the corresponding conditions and procedures specified in the applicable tso. eurocae concurs with rtca on the environmental conditions and test procedures set forth herein. [ 7] arp5412b, aircraft lightning environment and related test waveforms [ s]. the faa strongly encourages the use of rtca/ do- 160g for new articles. it includes 26 sections and three appendices, covering topics such as temperature, humidity, shock, vibration, power input, radio frequency, lightning, electrostatic discharge, and more. 1997 copies of this document may be obtained from rtca, inc. washington, dc 6. , suite 1020 washington, dcusa environmental conditions andtest procedures for airborne equipment j rtcaldo- 160d prepared by sc- 13 5 ortca, inc. rtca do- 160g is a standard document for testing airborne equipment for various aircraft types and environmental conditions. document history. home / products / do- 160g – electronic. download the full text or the do- 357 user guide from the web page. 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. rtca, incorporated is a not - for - profit corporation formed to advance the art and science of aviation and aviation electronic systems for th e benefit of the public. it is required to specify fluids used, test method and temperature of exposure in the test procedure and the environmental qualification form. 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. the generator output is measured and verified using the calibration loop on the injection transformer. partner sites youtube to mp3 converter about us. foreword this report was prepared by rtca special committee 135 ( sc- 135) and approved by the rtca program management committee ( pmc) on decem. 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. rtca, incorporated is a not- for- profit. environmental conditions and test procedures for airborne equipment. do- 160, environmental conditions and test procedures for airborne equipment is a standard for the environmental testing of avionics hardware. when approved by eurocae, this document will be identified jointly as rtca do - 160 g / eurocae ed - 14 g. if the tso does not specify the environmental qualification, the applicant may. finally, we will look at the future direction of sc- 135, and the timetable. rtca/ do- 160 ( or its precursor, rtca/ do- 138) has been used as a standard for environmental testing since 1958. it is published by the radio technical commission for aeronautics ( rtca) and supersedes do- 138. 1150 18th street, n. changes in each section since the release of do- 160f will be summarized. although an applicant may request to use an earlier version of do- 160, we recommend that you use rtca/ do- 160g. ac 21- 16g ( pdf). this document was prepared by special committee 135 ( scand was approved by the rtca program management committee ( pmc) on decem. the waveform verification set- up is shown in figure 22- 16 and is used during these tests. [ 8] arp5416a, aircraft lightning test methods [ s]. the course will provide an understanding of the use of do- 160g and how it fits in with the greater. rtca/ do- 160g environmental conditions and test procedures for airborne equipment, provides a laboratory means to determine the performance characteristics of airborne equipment.