Specifies a flexure test procedure for reconnectable and permanent hydraulik tube joints. This procedure is intended for conducting flexure tests on fittings with high-strength hydraulik tubes made of corrosion-resisting steel, nimonic, titanium and aluminium used on commercial and military aircraft.

General information

  • Status :  Withdrawn
    Publication date : 1996-01
  • Edition : 1
    Number of pages : 5
  • :
    ISO/TC 20/SC 10
    Aerospace fluid systems and components
  • 49.080
    Aerospace fluid systems and components

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