Standard Historical Last Updated: Aug 16, 2017 Track Document
ASTM F945-01

Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials

Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials F0945-01 ASTM|F0945-01|en-US Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials Standard new BOS Vol. 15.03 Committee F07
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Scope

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.

1.2 The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of prestressed titanium alloys to crack when subsequently heated to elevated temperatures.

1.3 Test conditions are based upon manufacturer's maximum recommended operating solution concentration.

1.4 This standard does not purport to address all of the safety problems associated with its use. It is the responsibility of whoever uses this standard to consult and establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific precautionary statements, see 5.3 and 5.6.

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Details
Book of Standards Volume: 15.03
Developed by Subcommittee: F07.07
Pages: 5
DOI: 10.1520/F0945-01
ICS Code: 49.025.30