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SAE ARP1795 Rev A

Current Revision

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

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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.

SDO SAE: SAE International
Document Number ARP1795
Publication Date Oct. 1, 1990
Language en - English
Page Count 6
Revision Level A
Supercedes
Committee
Publish Date Document Id Type View
Oct. 1, 1990 ARP1795A Revision