Description
1.1 This test method 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.
Product Details
- Published:
- 11/01/2012
- Number of Pages:
- 5
- File Size:
- 1 file , 89 KB
- Redline File Size:
- 2files, 220 KB
