The invention relates to a pipeline for conducting {HEAD ~ air}, in particular in {TAIL ~ 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 air conditioning in aircrafts 
in particular in
The invention relates to a pipeline for conducting { HEAD ~ air } , in particular in { TAIL ~ 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 air conditioning in aircrafts
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