ASTM F1111-08
(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, and X1.3.
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Designation:F 1111 – 08
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 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, opera-
specimens during the test and the ratio of area of immersed
tions, 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, and X1.3.
chosen as to withstand the resulting pressures.)
2. Referenced Documents 4.2 Constant Temperature Device—Any suitable regulated
2
heating device may be employed for maintaining the solution
2.1 ASTM Standards:
at the required temperature.
D 329 Specification for Acetone
4.3 Sandblaster.
D 740 Specification for Methyl Ethyl Ketone
4.4 Ampere Meter, capable of measuring 60 65A.
D 1193 Specification for Reagent Water
4.5 Oven, capable of maintaining temperature of 110 6 2°C
D 4080 Specification for Trichloroethylene, Technical and
(230 6 4°F).
Vapor-Degreasing Grade
4.6 Plating Bath, containing the solution specified in X1.2.
2.2 Industry Standards:
SAE-AMS-6345 Steel Sheet, Strip and Plate (SAE 4130)
5. Reagents
3
Normalized or Otherwise Heat Treated
5.1 PurityofWater—Unless otherwise indicated, references
3. Significance and Use to water shall be understood to mean reagent water as defined
by Type III of Specification D 1193.
3.1 The data generated by this test method shall be used to
5.2 Trichloroethylene, in accordance with Specification
determine whether low embrittling cadmium plated parts are
D 4080.
5.3 Methyl Ethyl Ketone, in accordance with Specification
1
D 740.
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
5.4 Acetone, in accordance with Specification D 329.
Qualification Testing of Aircraft Cleaning Materials.
5.5 Aluminum Oxide, 180 grit.
Current edition approved May 1, 2008. Published June 2008. Originally
approved in 1988. Last previous edition approved in 2002 as F 1111 – 02.
6. Safety Precautions
2
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
6.1 The solvents used in cleaning test specimens are flam-
Standards volume information, refer to the standard’s Document Summary page on
mable or harmful if inhaled, or both. Keep away from sparks
the ASTM website.
3 and open flames. Avoid breathing vapors and prolonged or
Available from Society of Automotive Engineers (SAE), 400 Commonwealth
Dr., Warrendale, PA 15096-0001. repeated contact with skin. Use adequate ventilation.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.
1
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F1111–08
6.2 Cyanides and cadmium oxide are very toxic and corro- 9.3 Temperature—Unless otherwise specified, the test tem-
sive to skin. Take suitable precautions in the handling of them perature shall be 35 6 1°C (95 6 2°F).
to avoid personal injury. Use adequate ventilation and keep 9.4 Test Duration—Unless otherwise specified, the test
away from acids. period shall be 24 h.
6.3 Some materials used for aircraft maintenance may
contain flammable solvents, acids or alkalis, or other toxic 10. Procedure
compounds. Take suitable
...
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:F1111–02 Designation:F 1111 – 08
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, and X1.3.
2. Referenced Documents
2
2.1 ASTM Standards:
D 329 Specification for Acetone
D 740 Specification for Methyl Ethyl Ketone
D 1193 Specification for Reagent Water
D 4080 Specification for Trichloroethylene, Technical and Vapor-Degreasing Grade
2.2 Industry Standards:
3
SAE-AMS-6345 Steel Sheet, Strip and Plate (SAE 4130) Normalized or Otherwise Heat Treated
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.
4.4 Ampere Meter, capable of measuring 60 65A.
4.5 Oven, capable of maintaining temperature of 110 6 2°C (230 6 4°F).
4.6 Plating Bath, containing the solution specified in X1.2.
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.
Current edition approved May 10, 2002. Published June 2002. Originally published as F1111–88. Last previous edition F1111–88 (1998).
Current edition approved May 1, 2008. Published June 2008. Originally approved in 1988. Last previous edition approved in 2002 as F 1111 – 02.
2
For referencedASTM standards, visit theASTM website, www.astm.org, or contactASTM Customer Service at service@astm.org. ForAnnualBookofASTMStandards
, Vol 06.04.volume information, refer to the standard’s Document Summary page on the ASTM website.
3
Annual Book of ASTM Standards, Vol 11.01.
3
Available from Society of Automotive Engineers (SAE), 400 Commonwealth Dr., Warrendale, PA 15096-0001.
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.
1
---------------------- Page: 1 ----------------------
F1111–08
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.
5.2 Trichloroethylene, in accordance with Specification D 4080.
5.3 Methyl Ethyl Ketone, in accordance with Specification D 740.
5.4 Acetone, in accordance with Specification D 329.
5.5 Aluminum 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 breathing vapors and prolonged or repeated contact with skin. Use adequate ventilation.
6.2 Cyanidesandcadmiumoxideareverytoxicandcorrosiv
...
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