Abstract

Gives characteristics of these assemblies for use in aircraft fluid systems at temperatures between -55 and +200 °C and at nominal pressures, depending on bore size, up to 6,8 MPa. Special approval from the proper national authority may be required it these hoses are to be part of a pressurized gas storage system. Two types of hose assembly are covered: Typ 1 - non-conductive inner tube and type 2 - conductive inner tube.


General information 

  • Status
     : Withdrawn
    Publication date
     : 1984-03
  • Edition
     : 1
    Number of pages
     : 8
  • Technical Committee
     : ISO/TC 20/SC 10 Aerospace fluid systems and components
  • ICS
     :
    49.080 Aerospace fluid systems and components
    83.140.40 Hoses

Life cycle

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