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.
Текущий статус : WithdrawnДата публикации : 1996-01
Версия : 1
Технический комитет:Aerospace fluid systems and components