ASTM F1111-88(1998)
Historical Standard: ASTM F1111-88(1998) Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
SUPERSEDED (see Active link, below)
ASTM F1111
1. Scope
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, and X1.3.
2. Referenced Documents (purchase separately) The documents listed below are referenced within the subject standard but are not provided as part of the standard.
ASTM Standards
D329 Specification for Acetone
D1193 Specification for Reagent Water
Industry Standards
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.Military Standards
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.milKeywords
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 Code
ICS Number Code 49.025.99 (Other materials)
DOI: 10.1520/F1111-88R98
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