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ARP1795A - Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials

Details
Document Number: ARP1795A
Revision Number: A
Title
Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials
Scope
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.
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