ASTM F1111-08b(2019)
(Test Method)Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
SIGNIFICANCE AND USE
3.1 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.
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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements see Section 6, 4.1.
1.3 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
General Information
- Status
- Published
- Publication Date
- 14-Nov-2019
- Technical Committee
- F07 - Aerospace and Aircraft
- Drafting Committee
- F07.07 - Qualification Testing of Aircraft Cleaning Materials
Relations
- Effective Date
- 15-Nov-2019
- Effective Date
- 01-Jun-2007
- Effective Date
- 01-Jun-2007
- Effective Date
- 01-Mar-2006
- Effective Date
- 10-Dec-2002
- Effective Date
- 10-Dec-1999
- Effective Date
- 10-Feb-1999
- Effective Date
- 10-Feb-1999
- Effective Date
- 15-Nov-2019
Overview
ASTM F1111-08b(2019) is the Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals. Issued by ASTM International, this standard provides a quantitative testing procedure to determine how aircraft maintenance chemicals affect the corrosion resistance of low-embrittling cadmium plating applied to high-strength steel parts used in aviation. The primary intent is to help assess, under controlled laboratory conditions, whether such plated parts are susceptible to corrosion or damage during typical maintenance processes using these chemicals.
This international standard was developed in accordance with recognized rules, supporting consistency and harmonization in aerospace corrosion testing worldwide.
Key Topics
- Corrosion Testing: Establishes a consistent test method using total immersion and controlled conditions to evaluate potential weight loss of cadmium-coated steel, indicating corrosion.
- Aircraft Maintenance Chemicals: Focuses specifically on chemicals commonly used in aircraft cleaning and maintenance.
- Material Compatibility: Assesses compatibility of maintenance chemicals with cadmium-plated high-strength steel parts, vital for aircraft reliability and safety.
- Measurement and Reporting: Requires quantitative measurement of specimen weight before and after exposure, with detailed reporting of weight loss and visual changes.
- Safety Precautions: Emphasizes the need for appropriate health, safety, and environmental practices due to the potential hazards involved in the test.
- International Harmonization: Developed under WTO TBT Committee principles, ensuring global relevance.
Applications
The ASTM F1111 standard is widely used in the aerospace industry and by maintenance facilities to:
- Qualify Aircraft Maintenance Chemicals: Determine if cleaning chemicals, solvents, or degreasers can be safely used on cadmium-plated components without causing unacceptable corrosion or degradation.
- Support Product Approvals: Provide data required by manufacturers, maintenance providers, and regulatory agencies when approving new aircraft maintenance materials.
- Assist Regulatory Compliance: Aligns with requirements from organizations like the U.S. Department of Defense and references industry and military specifications (e.g., MIL-STD-870, SAE-AMS-6345).
- Guide Maintenance Best Practices: Establish protocols for choosing chemicals that minimize corrosion risks, extending the operational life of components and enhancing aviation safety.
- Material & Process Evaluation: Useful for validating updates to plating processes, verifying consistency of cadmium coatings, and ensuring ongoing compliance with industry standards.
Related Standards
- MIL-STD-870: Cadmium Plating, Low Embrittlement, Electrodeposition - Specifies requirements for the plating applied to test specimens.
- SAE-AMS-6345: Steel Sheet, Strip, and Plate (SAE 4130) - Specifies the material used for preparing test samples.
- ASTM D329: Specification for Acetone - Reference for reagent used in the cleaning of specimens.
- ASTM D1193: Specification for Reagent Water - Defines water quality requirements for laboratory testing.
Other related ASTM standards cover corrosion testing, chemical compatibility testing, and plating methods for metal components in aerospace and defense sectors.
Practical Value
By enabling quantitative evaluation of corrosion effects, ASTM F1111 supports the development and selection of maintenance chemicals that do not compromise the integrity of cadmium-plated aircraft parts. With standardized reporting and enhanced safety protocols, this test method contributes directly to preventive maintenance strategies, reduced material failure rates, and improved operator safety within the aviation industry. Adopting this standard ensures consistency, traceability, and international acceptance of test results, helping organizations meet stringent quality and regulatory requirements.
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Frequently Asked Questions
ASTM F1111-08b(2019) is a standard published by ASTM International. Its full title is "Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals". This standard covers: SIGNIFICANCE AND USE 3.1 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. 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements see Section 6, 4.1. 1.3 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
SIGNIFICANCE AND USE 3.1 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. 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements see Section 6, 4.1. 1.3 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
ASTM F1111-08b(2019) is classified under the following ICS (International Classification for Standards) categories: 49.025.99 - Other materials. The ICS classification helps identify the subject area and facilitates finding related standards.
ASTM F1111-08b(2019) has the following relationships with other standards: It is inter standard links to ASTM F1111-08b(2013), ASTM D329-07, ASTM D329-07e1, ASTM D1193-06, ASTM D329-02, ASTM D329-99, ASTM D1193-99, ASTM D1193-99e1, ASTM D6361/D6361M-98(2020). Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
ASTM F1111-08b(2019) is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the
Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Designation: F1111 − 08b (Reapproved 2019)
Standard Test Method for
Corrosion of Low-Embrittling Cadmium Plate by Aircraft
Maintenance Chemicals
This standard is issued under the fixed designation F1111; the number immediately following the designation indicates the year of
original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A
superscript epsilon (´) indicates an editorial change since the last revision or reapproval.
This standard has been approved for use by agencies of the U.S. Department of Defense.
1. Scope 2.3 Military Standards:
MIL-STD-870 Cadmium Plating, Low Embrittlement, Elec-
1.1 This test method is intended as a means of determining
trodeposition
the corrosive effects of aircraft maintenance chemicals on
low-embrittlingcadmiumplatingusedonaircrafthigh-strength
3. Significance and Use
steel, under conditions of total immersion by quantitative
3.1 The data generated by this test method shall be used to
measurements of weight change.
determine whether low embrittling cadmium plated parts are
1.2 This standard may involve hazardous materials, liable to be corroded or damaged by application of the test
material during routine maintenance operations.
operations, and equipment. This standard does not purport to
address all of the safety concerns, if any, associated with its
4. Apparatus
use. It is the responsibility of the user of this standard to
4.1 Wide Mouth Sealable Glass Jar or Stoppered Flask,
establish appropriate safety, health, and environmental prac-
having a capacity so chosen that specimens will remain fully
tices and determine the applicability of regulatory limitations
immersed in a vertical position and not in contact with other
prior to use. For specific hazard statements see Section 6, 4.1.
specimens during the test and the ratio of area of immersed
1.3 This international standard was developed in accor-
metal to the volume of solution will be as prescribed in 9.1.
dance with internationally recognized principles on standard-
(Warning—Some aircraft maintenance chemicals when
ization established in the Decision on Principles for the
heated have high vapor pressures or may produce gases during
Development of International Standards, Guides and Recom-
testing. Suitable precautions should be taken to prevent the
mendations issued by the World Trade Organization Technical
containing vessel from exploding or the vessel should be so
Barriers to Trade (TBT) Committee.
chosen as to withstand the resulting pressures.)
4.2 Constant Temperature Device—Any suitable regulated
2. Referenced Documents
heating device may be employed for maintaining the solution
2.1 ASTM Standards:
at the required temperature.
D329 Specification for Acetone
4.3 Oven, capable of maintaining temperature of 110 6
D1193 Specification for Reagent Water
2 °C (230 6 4 °F).
2.2 Industry Standards:
5. Reagents
SAE-AMS-6345 Steel Sheet, Strip and Plate (SAE 4130)
Normalized or Otherwise Heat Treated
5.1 Purity of Water—Unless otherwise indicated, references
to water shall be understood to mean reagent water as defined
by Type III of Specification D1193.
This test method is under the jurisdiction of ASTM Committee F07 on
5.2 Methyl n-propyl ketone (MPK).
Aerospace and Aircraft and is the direct responsibility of Subcommittee F07.07 on
5.3 Acetone, in accordance with Specification D329.
Qualification Testing of Aircraft Cleaning Materials.
Current edition approved Nov. 15, 2019. Published December 2019. Originally
approved in 1988. Last previous edition approved in 2013 as F1111 – 08b(2013).
6. Safety Precautions
DOI: 10.1520/F1111-08BR19.
2 6.1 The solvents used in cleaning test specimens are flam-
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
mable or harmful if inhaled, or both. Keep away from sparks
Standards volume information, refer to the standard’s Document Summary page on
the ASTM website.
Available from Society of Automotive Engineers (SAE), 400 Commonwealth Available from the Department of Defense Single Stock Point (DODSSP); web
Dr., Warrendale, PA 15096-0001. server at http://dodssp.daps.dla.mil
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
F1111 − 08b (2019)
and open flames. Avoid breathing vapors and prolonged or 9.3 Temperature—Unless otherwise specified, the test tem-
repeated contact with skin. Use adequate ventilation. perature shall be 35 6 1 °C (95 6 2 °F).
6.2 Some materials used for aircraft maintenance may 9.4 Test Duration—Unless otherwise specified, the test pe-
contain flammable solvents, acids or alkalis, or other toxic riod s
...




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