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ASTM F945-98

Historical Revision

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

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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.


SDO ASTM: ASTM International
Document Number F945
Publication Date Nov. 10, 2001
Language en - English
Page Count 5
Revision Level 98
Supercedes
Committee F07.07
Publish Date Document Id Type View
Sept. 1, 2022 F0945-22 Revision
Nov. 1, 2012 F0945-12 Revision
April 1, 2006 F0945-06 Revision
Nov. 10, 2001 F0945-98 Revision
Nov. 10, 2001 F0945-01 Revision
May 1, 2019 F0945-12R19 Reaffirmation