This standard was last reviewed and confirmed in 2019. Therefore this version remains current.
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.
Status : PublishedPublication date : 1984-03
Edition : 1Number of pages : 8
Technical Committee:Aerospace fluid systems and components
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