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