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: WithdrawnPublication date: 1984-03
Edition: 1Number of pages: 8
Technical Committee: ISO/TC 20/SC 10 Aerospace fluid systems and components
ISO 7313:1984Stage: 95.99
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