This specification covers the engineering requirements for producing brazed joints using an aluminum alloy with melting point below that of the basis metal as the brazing filler metal.
This specification covers the engineering requirements for production of brazed joints using an aluminum alloy with melting point below that of the basis metal as the brazing filler metal.
This recommended practice establishes procedures for the application of long string abrasive fibers to machined aircraft structures for the purpose of removing burrs produced during the machining operations. This procedure is applicable to aluminum, titanium, and steel.