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: WithdrawnPublication date: 1984-03Stage: Withdrawal of International Standard [95.99]
-
Edition: 1Number of pages: 8
-
Technical Committee :ISO/TC 20/SC 10
- RSS updates
Life cycle
-
Now
-
Revised by
PublishedISO 7313:2020