Specifies procedures to determine and classify the fatigue strength of reconnectable or permanent hydraulic tube joints. The procedure is intended for conducting flexure tests of these parts with high strength tubes of various alloys such as corrosion resistant steel, Nimonic, titanium and aluminium alloy tube for use on commercial and military aircraft.
Текущий статус : WithdrawnДата публикации : 1983-07
Версия : 1
Технический комитет:Aerospace fluid systems and components