SAE AS3412, revision A
Bolt, Tee Head, Ams 5662, Chamfered, .375-24unjf-3a (Stress Rupture Resistant)
Month of publication: 2001-10-01
Developed by committee: E-25 General Standards For Aerospace And Propulsion Systems
Annotation and contents
Source of this annotation and contents: SAE.
No scope available.
