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ASTM F1111-08b

(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
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 and health practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements see Section 6, 4.1.

General Information

Status
Historical
Publication Date
30-Nov-2008
ICS
49.025.99 - Other materials
Technical Committee
F07 - Aerospace and Aircraft
Drafting Committee
F07.07 - Qualification Testing of Aircraft Cleaning Materials
Current Stage
Ref Project

Relations

Replaces
ASTM F1111-08a - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
Effective Date
01-Dec-2008
Replaced By
ASTM F1111-08b(2013) - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
Effective Date
01-Dec-2013
Referred By
ASTM D6361/D6361M-98(2020) - Standard Guide for Selecting Cleaning Agents and Processes
Effective Date
01-Dec-2008

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ASTM F1111-08b - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance ChemicalsASTM F1111-08b - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
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REDLINE ASTM F1111-08b - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance ChemicalsREDLINE ASTM F1111-08b - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
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REDLINE ASTM F1111-08b - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance ChemicalsREDLINE ASTM F1111-08b - Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals
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Standards Content (Sample)

NOTICE: This standard has either been superseded and replaced by a new version or withdrawn.
Contact ASTM International (www.astm.org) for the latest information
Designation: F1111 − 08b
StandardTest Method for
Corrosion of Low-Embrittling Cadmium Plate by Aircraft
1
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 Department of Defense.
1. Scope 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
4. Apparatus
low-embrittlingcadmiumplatingusedonaircrafthigh-strength
4.1 Wide Mouth Sealable Glass Jar or Stoppered Flask,
steel, under conditions of total immersion by quantitative
having a capacity so chosen that specimens will remain fully
measurements of weight change.
immersed in a vertical position and not in contact with other
1.2 This standard may involve hazardous materials,
specimens during the test and the ratio of area of immersed
operations, and equipment. This standard does not purport to
metal to the volume of solution will be as prescribed in 9.1.
address all of the safety concerns, if any, associated with its
(Warning—Some aircraft maintenance chemicals when
use. It is the responsibility of the user of this standard to
heated have high vapor pressures or may produce gases during
establish appropriate safety and health practices and deter-
testing. Suitable precautions should be taken to prevent the
mine the applicability of regulatory limitations prior to use.
containing vessel from exploding or the vessel should be so
For specific hazard statements see Section 6, 4.1.
chosen as to withstand the resulting pressures.)
4.2 Constant Temperature Device—Any suitable regulated
2. Referenced Documents
2 heating device may be employed for maintaining the solution
2.1 ASTM Standards:
at the required temperature.
D329 Specification for Acetone
D1193 Specification for Reagent Water 4.3 Oven, capable of maintaining temperature of 110 6 2°C
(230 6 4°F).
2.2 Industry Standards:
SAE-AMS-6345 Steel Sheet, Strip and Plate (SAE 4130)
5. Reagents
3
Normalized or Otherwise Heat Treated
5.1 Purity of Water—Unless otherwise indicated, references
2.3 Military Standards:
to water shall be understood to mean reagent water as defined
MIL-STD-870 Cadmium Plating, Low Embrittlement, Elec-
4
by Type III of Specification D1193.
trodeposition
5.2 Methyl n-propyl ketone (MPK).
3. Significance and Use
5.3 Acetone, in accordance with Specification D329.
3.1 The data generated by this test method shall be used to
determine whether low embrittling cadmium plated parts are
6. Safety Precautions
6.1 The solvents used in cleaning test specimens are flam-
1
mable or harmful if inhaled, or both. Keep away from sparks
This test method is under the jurisdiction of ASTM Committee F07 on
Aerospace and Aircraft and is the direct responsibility of Subcommittee F07.07 on
and open flames. Avoid breathing vapors and prolonged or
Qualification Testing of Aircraft Cleaning Materials.
repeated contact with skin. Use adequate ventilation.
Current edition approved Dec. 1, 2008. Published January 2009. Originally
approved in 1988. Last previous edition approved in 2008 as F1111 – 08a. DOI:
6.2 Some materials used for aircraft maintenance may
10.1520/F1111-08B.
contain flammable solvents, acids or alkalis, or other toxic
2
For referenced ASTM standards, visit the ASTM website, www.astm.org, or
compounds. Take suitable precautions to prevent personal
contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
Standards volume information, refer to the standard’s Document Summary page on injury.
the ASTM website.
3
Available from Society of Automotive Engineers (SAE), 400 Commonwealth 7. Test Specimens
Dr., Warrendale, PA 15096-0001.
4
7.1 The test specimens shall be made of 4130 steel Condi-
Available from the Department of Defense Single Stock Point (DODSSP); web
server at http://dodssp.daps.dla.mil tion N in accordance with SAE-AMS-6345, measuring 25.4 by
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
1

---------------------- Page: 1 ----------------------
F1111 − 08b
50.8 by 1.22 mm (1 by 2 by 0.048 in.) and cadmium plated in 10. Procedure
accordance with MIL-STD-870, Type I, Class1.
10.1 Dry the precleaned specimens at 110°C (230°F) for 1
7.2 Three replicates should be tested in each concentration h, allow to cool to room temperature in a desiccator, then
of maintenance chemicals solution as prescribed in 9.2. weigh
...

This document is not anASTM standard and is intended only to provide the user of anASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation:F1111–08a Designation:F 1111 – 08b
Standard Test Method for
Corrosion of Low-Embrittling Cadmium Plate by Aircraft
1
Maintenance Chemicals
This standard is issued under the fixed designation F 1111; 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 Department of Defense.
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.
2. Referenced Documents
2
2.1 ASTM Standards:
D 329 Specification for Acetone D740Specification for Methyl Ethyl Ketone
D 1193 Specification for Reagent Water
D4080Specification for Trichloroethylene, Technical and Vapor-Degreasing Grade Specification for Reagent Water
2.2 Industry Standards:
3
SAE-AMS-6345 Steel Sheet, Strip and Plate (SAE 4130) Normalized or Otherwise Heat Treated
2.3 Military Standards:
4
MIL-STD-870 Cadmium Plating, Low Embrittlement, Electrodeposition
3. 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.
4. Apparatus
4.1 WideMouthSealableGlassJarorStopperedFlask, having a capacity so chosen that specimens will remain fully immersed
in a vertical position and not in contact with other specimens during the test and the ratio of area of immersed metal to the volume
of solution will be as prescribed in 9.1. ( Warning—Some aircraft maintenance chemicals when heated have high vapor pressures
or may produce gases during testing. Suitable precautions should be taken to prevent the containing vessel from exploding or the
vessel should be so chosen as to withstand the resulting pressures.)
4.2 Constant Temperature Device—Any suitable regulated heating device may be employed for maintaining the solution at the
required temperature.
4.3 Sandblaster.
4.4Ampere Meter, capable of measuring 60 65A.
4.5Oven, capable of maintaining temperature of 110 6 2°C (230 6 4°F).
4.6Plating Bath, containing the solution specified in MIL-STD-870, Type I, Class 1.
1
This test method is under the jurisdiction ofASTM Committee F07 onAerospace andAircraft and is the direct responsibility of Subcommittee F07.07 on Qualification
Testing of Aircraft Cleaning Materials.
CurrenteditionapprovedOct.Dec.1,2008.PublishedNovember2008.January2009.Originallyapprovedin1988.Lastpreviouseditionapprovedin2008asF 1111 – 08a.
2
For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at service@astm.org. ForAnnualBookofASTMStandards
volume information, refer to the standard’s Document Summary page on the ASTM website.
3
Available from Society of Automotive Engineers (SAE), 400 Commonwealth Dr., Warrendale, PA 15096-0001.
4
Methyl-n-propyl ketone, 90% purity or better
4
Available from the Department of Defense Single Stock Point (DODSSP); web server at http://dodssp.daps.dla.mil
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.
1

---------------------- Page: 1 ----------------------
F 1111 – 08b
5. Reagents
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 D 1193.
5.2Trichloroethylene, in accordance with Specification D4080.
5.2 Methyl n-propyl ketone (MPK).
5.3 Methyl Ethyl Ketone, in accordance with Specification D740.
5.4Acetone, in accordance with Specification D 329.
5.5Aluminum Oxide, 180 grit.
6. Safety Precautions
6.1 The solvents used in cleaning test specimens are flammable or harmful if inhaled, or both. Keep away from sparks and open
flames. Avoid
...

This document is not anASTM standard and is intended only to provide the user of anASTM standard an indication of what changes have been made to the previous version. Because
it may not be technically possible to adequately depict all changes accurately, ASTM recommends that users consult prior editions as appropriate. In all cases only the current version
of the standard as published by ASTM is to be considered the official document.
Designation:F1111–08a Designation:F 1111 – 08b
Standard Test Method for
Corrosion of Low-Embrittling Cadmium Plate by Aircraft
1
Maintenance Chemicals
This standard is issued under the fixed designation F 1111; 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 Department of Defense.
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.
2. Referenced Documents
2
2.1 ASTM Standards:
D 329 Specification for Acetone D740Specification for Methyl Ethyl Ketone
D 1193 Specification for Reagent Water
D4080Specification for Trichloroethylene, Technical and Vapor-Degreasing Grade Specification for Reagent Water
2.2 Industry Standards:
3
SAE-AMS-6345 Steel Sheet, Strip and Plate (SAE 4130) Normalized or Otherwise Heat Treated
2.3 Military Standards:
4
MIL-STD-870 Cadmium Plating, Low Embrittlement, Electrodeposition
3. 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.
4. Apparatus
4.1 WideMouthSealableGlassJarorStopperedFlask, having a capacity so chosen that specimens will remain fully immersed
in a vertical position and not in contact with other specimens during the test and the ratio of area of immersed metal to the volume
of solution will be as prescribed in 9.1. ( Warning—Some aircraft maintenance chemicals when heated have high vapor pressures
or may produce gases during testing. Suitable precautions should be taken to prevent the containing vessel from exploding or the
vessel should be so chosen as to withstand the resulting pressures.)
4.2 Constant Temperature Device—Any suitable regulated heating device may be employed for maintaining the solution at the
required temperature.
4.3 Sandblaster.
4.4Ampere Meter, capable of measuring 60 65A.
4.5Oven, capable of maintaining temperature of 110 6 2°C (230 6 4°F).
4.6Plating Bath, containing the solution specified in MIL-STD-870, Type I, Class 1.
1
This test method is under the jurisdiction ofASTM Committee F07 onAerospace andAircraft and is the direct responsibility of Subcommittee F07.07 on Qualification
Testing of Aircraft Cleaning Materials.
CurrenteditionapprovedOct.Dec.1,2008.PublishedNovember2008.January2009.Originallyapprovedin1988.Lastpreviouseditionapprovedin2008asF 1111 – 08a.
2
For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at service@astm.org. ForAnnualBookofASTMStandards
volume information, refer to the standard’s Document Summary page on the ASTM website.
3
Available from Society of Automotive Engineers (SAE), 400 Commonwealth Dr., Warrendale, PA 15096-0001.
4
Methyl-n-propyl ketone, 90% purity or better
4
Available from the Department of Defense Single Stock Point (DODSSP); web server at http://dodssp.daps.dla.mil
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.
1

---------------------- Page: 1 ----------------------
F 1111 – 08b
5. Reagents
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 D 1193.
5.2Trichloroethylene, in accordance with Specification D4080.
5.2 Methyl n-propyl ketone (MPK).
5.3 Methyl Ethyl Ketone, in accordance with Specification D740.
5.4Acetone, in accordance with Specification D 329.
5.5Aluminum Oxide, 180 grit.
6. Safety Precautions
6.1 The solvents used in cleaning test specimens are flammable or harmful if inhaled, or both. Keep away from sparks and open
flames. Avoid
...

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ASTM E285-08(2020)(Test Method)
Standard Test Method for Oxyacetylene Ablation Testing of Thermal Insulation Materials

SIGNIFICANCE AND USE
4.1 This test method is intended to screen the most obvious poor materials from further consideration. Since the combustion gases more closely resemble the environment generated in rocket motors, this test method is more applicable to screening materials for nozzles and motor liners than for aerodynamic heating.  
4.2 The environment for any specific high-temperature thermal protection problem is peculiar to that particular application. The conditions generated by the oxyacetylene heat source in this test method represent only one set of conditions; they do not simulate any specific application. Thus, the test results cannot be used to predict directly the behavior of materials for specific environments, nor can they be used for design purposes. However, over a number of years, the test has been useful in determining the relative merit of materials, particularly in weeding out obviously poor materials from more advanced data-generation programs. It has also been considered for use as a production quality-control test for rocket insulation materials.  
4.3 The tester is cautioned to use prudence in extending the usefulness of the test method beyond its original intent, namely, screening. For situations having environments widely different from those of the test, the user is urged to modify the oxyacetylene burner conditions to suit his requirements or perhaps change to a different heat-generating device that provides better simulation.
SCOPE
1.1 This test method covers the screening of ablative materials to determine the relative thermal insulation effectiveness when tested as a flat panel in an environment of a steady flow of hot gas provided by an oxyacetylene burner.  
1.2 This test method should be used to measure and describe the properties of materials, products, or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard of materials, products, or assemblies under actual fire conditions. However, results of this test method may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.  
1.3 The values stated in SI units are to be regarded as the standard.  
1.4 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.  
1.5 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.

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ASTM
ASTM F1111-08b(2019)(Test Method)
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.

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ASTM E1731-11(2018)(Test Method)
Standard Test Method for Gravimetric Determination of Nonvolatile Residue from Cleanroom Gloves

SIGNIFICANCE AND USE
5.1 The NVR obtained by this test method is that amount which is available for release by the gloves onto handled surfaces.  
5.2 Evaporation of solvent at the stated temperature is to quantify the NVR that can be expected to exist at room temperature, since the slight difference between room temperature and the test temperature is not likely to result in significant variances.  
5.3 This method may be more aggressive than necessary to determine the suitability of cleanroom gloves that are restricted to dry operations only.  
5.4 Various other methods exist for determining NVR, for example Practice G120 and IEST-RP-CC005. This test is not intended to replace test methods used for other purposes.
SCOPE
1.1 This test method covers the determination of solvent extractable nonvolatile residue (NVR) from gloves used in cleanrooms where spacecraft are assembled, cleaned, or tested.  
1.2 The NVR of interest is that which can be extracted from gloves using a specified solvent that has been selected for its extracting qualities, or because it is representative of solvents used in the particular facility. Alternative solvents may be used, but since their use may result in different values being generated, they must be identified in the procedure data sheet.  
1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.  
1.4 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.  
1.5 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.

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ASTM
ASTM E1560-18(Test Method)
Standard Test Method for Gravimetric Determination of Nonvolatile Residue From Cleanroom Wipers

SIGNIFICANCE AND USE
5.1 The NVR obtained by this test method is that amount which is available for release by wipers in normal use.  
5.2 Evaporation of the solvent at the stated temperature is to quantify the NVR that can be expected to exist at room temperature, since the slight difference between room temperature and test temperature has not been shown to result in significant variances.  
5.3 This test method may be more aggressive than necessary for the evaluation of wipers that will be restricted to dry use only.  
5.4 Numerous other methods are being used to determine NVR. This test method is not intended to replace test methods used for other applications.
SCOPE
1.1 This test method covers the determination of solvent extractable nonvolatile residue (NVR) from wipers used in assembly, cleaning, or testing of spacecraft, but not from those used for analytical surface sampling of hardware.  
1.2 The NVR of interest is that which can be extracted from cleanroom wipers using a specified solvent that has been selected for its extractive qualities. Alternative solvents may be selected, but since their use may result in different values being generated, they must be identified in the procedure data sheet.  
1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.  
1.3.1 Exception—The inch-pound units are included for information only.  
1.4 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.  
1.5 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.

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  • Standard
    5 pages
    English language
    sale 15% off