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.
| SAE International | |
|---|---|
| Product Category | Standards and Technical Documents |
| Product Number | ARP1795A |
| Product Name | Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials |
