The invention relates to a pipeline for conducting air, in particular in a temperature range between −55° C. and +85° C. and at a differential pressure load of at most ±500 hPa relative to cabin pressure, for {HEAD ~ air conditioning} in {TAIL ~ aircrafts} 
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The invention relates to a pipeline for conducting air , in particular in a temperature range between −55 ° C. and +85 ° C. and at a differential pressure load of at most ±500 hPa relative to cabin pressure , for { HEAD ~ air conditioning } in { TAIL ~ aircrafts }
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