Abstract 

Covers Class I fitting assemblies of corrosion-resistant steel or titanium parts (- 55 °C to + 232 °C) and Class II fitting assemblies of corrosion-resistant steel and aluminium parts, DN 12 and larger (- 55 °C to + 135 °C) for use in aircraft hydraulic, fuel and lubricating oil systems and in aerospace pneumatic systems where some gaseous diffusion through the wall may be tolerated. Annex A gives equivalent materials and components for information only.


General information

  • Status :  Withdrawn
    Publication date : 1992-06
  • Edition : 1
    Number of pages : 14
  • :
    ISO/TC 20/SC 10
    Aerospace fluid systems and components
  • 49.080
    Aerospace fluid systems and components
    83.140.40
    Hoses

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