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