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:
2 files , 220 KB
Note:
This product is unavailable in Russia, Ukraine, Belarus
