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ASTM-F945 2006

$40.63

F945-06 Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials

Published By Publication Date Number of Pages
ASTM 2006 5
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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.

This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific precautionary statements, see and .

PDF Catalog

PDF Pages PDF Title
1 Scope
Referenced Documents
Significance and Use
Apparatus
2 Reagents and Materials
Precleaning Test Specimens
Specimen Fabrication
FIG. 1
3 (See

.)
FIG. 2
FIG. 3
FIG. 4

4 Determination of Test Results
Report
Precision and Bias
Keywords
A1. PRECAUTIONARY STATEMENTS
A1.1 Solvent (Typical for Toluene)
A1.2 Nitric Acid (Concentrated)
A1.3 Hydrofluoric Acid (concentrated)
ASTM-F945 2006
$40.63