Significance and Use
The data generated by this test method shall be used to determine whether low embrittling cadmium plated parts are liable to be corroded or damaged by application of the test material during routine maintenance operations.
1.1 This test method is intended as a means of determining the corrosive effects of aircraft maintenance chemicals on low-embrittling cadmium plating used on aircraft high-strength steel, under conditions of total immersion by quantitative measurements of weight change.
1.2 This standard may involve hazardous materials, operations, and equipment. 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 hazard statements see Section 6, 4.1.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
D329 Specification for Acetone
D1193 Specification for Reagent Water
SAE-AMS-6345 Steel Sheet, Strip and Plate (SAE 4130) Normalized or Otherwise Heat Treated Available from Society of Automotive Engineers (SAE), 400 Commonwealth Dr., Warrendale, PA 15096-0001.
MIL-STD-870 Cadmium Plating, Low Embrittlement, Electrodeposition Available from the Department of Defense Single Stock Point (DODSSP); web server at http://dodssp.daps.dla.mil
aircraft maintenance chemicals; corrosion; low-embrittling cadmium plate; weight loss; Aircraft chemicals/processes; Aircraft materials/applications (corrosion testing); Cadmium metals (coating/plating); Corrosion--aircraft metals; Embrittlement; Immersion--aircraft materials;
ICS Number Code 49.025.99 (Other materials)
ASTM International is a member of CrossRef.
Citing ASTM Standards
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