ARP1795 STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials
Revised
04/01/1982
- Features
- Issuing Committee
- Content
- This recommended practice 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.
- Pages
- 6
- Citation
- SAE International Recommended Practice, STRESS-CORROSION OF TITANIUM ALLOYS Effect of Cleaning Agents on Aircraft Engine Materials, SAE Standard ARP1795, Issued April 1982, https://doi.org/10.4271/ARP1795.