Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials(Cancelled Oct 1990) ARP1795A

This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.