Abstract

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     : Withdrawn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
  • Technical Committee
     : ISO/TC 20/SC 10 Aerospace fluid systems and components
  • ICS
     :
    49.080 Aerospace fluid systems and components

Life cycle

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