SAE ARP1795A
Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials(Cancelled Oct 1990)
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.
History:Standard | Published | Revision | Status |
---|---|---|---|
ARP1795A | 1990-10-01 | Latest | |
ARP1795 | 1982-04-01 | Historical |