This procurement specification covers aircraft-quality bolts and screws made of 6.0Al-4.0V titanium alloy and of 160 ksi tensile strength at room temperature. Updated para 3.5 by adding “two to” three threads in agreement with NASM1312-8 test methodology. Added additional difinitions to para 2.2. General updating for SAE requirements for obsolete specifications and standards.
Bolts and Screws, Titanium Alloy 6.0Al – 4.0V Procurement Specification For
2009-12-09
Conference paper
English
Bolts and Screws, Titanium Alloy 6.0Al - 4.0V Procurement Specification For
SAE Technical Papers | 2015
Bolts and Screws, Titanium Alloy 6.0Al - 4.0V Procurement Specification For
SAE Technical Papers | 2017
TITANIUM ALLOY CASTINGS, INVESTMENT 6.0Al - 4.0V Annealed
SAE Technical Papers | 1980
Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Annealed
SAE Technical Papers | 2017
Titanium Alloy Bars, Forgings and Forging Stock 6.0Al - 4.0V Annealed
SAE Technical Papers | 2007