ASTM F1110-2008 Standard Test Method for Sandwich Corrosion Test.pdf
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1、Designation: F 1110 08Standard Test Method forSandwich Corrosion Test1This standard is issued under the fixed designation F 1110; the number immediately following the designation indicates the year oforiginal adoption or, in the case of revision, the year of last revision. A number in parentheses in
2、dicates the year of last reapproval. Asuperscript 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. Scope1.1 This test method defines the procedure for evaluatingthe corrosivity of aircra
3、ft maintenance chemicals, when presentbetween faying surfaces (sandwich) of aluminum alloys com-monly used for aircraft structures. This test method is intendedto be used in the qualification and approval of compoundsemployed in aircraft maintenance operations.1.2 The values stated in SI units are t
4、o be regarded as thestandard. The values given in parentheses are for information.1.3 This standard may involve hazardous materials, opera-tions, and equipment. This standard does not purport toaddress all of the safety concerns, if any, associated with itsuse. It is the responsibility of the user o
5、f this standard toestablish appropriate safety and health practices and deter-mine the applicability of regulatory limitations prior to use.Specific hazard statements appear in Section 9.2. Referenced Documents2.1 ASTM Standards:2D 1193 Specification for Reagent WaterD 1748 Test Method for Rust Prot
6、ection by Metal Preser-vatives in the Humidity CabinetG46 Guide for Examination and Evaluation of PittingCorrosion2.2 Industry Standards:3SAE-AMS-QQ-A-250/4 Al Alloy 2024, Plate and SheetSAE-AMS-QQ-A-250/5 Al Alloy Alclad 2024, Plate andSheetSAE-AMS-QQ-A-250/12 Al Alloy 7075, Plate and SheetSAE-AMS-
7、QQ-A-250/13 Al Alloy Alclad 7075, Plate andSheet2.3 Military Specification:MIL-A-8625 Anodic Coatings for Aluminum and Al Al-loys43. Terminology3.1 Definition of Term Specific to This Standard:3.1.1 sandwich corrosion testa comparative acceleratedenvironmental test of the corrosivity of liquid or so
8、lid materialspresent between faying surfaces of structural aluminum alloyscommonly used in aerospace construction.4. Summary of Test Method4.1 Aluminum coupons having clad or anodized noncladsurfaces are sandwiched together with a filter paper saturatedwith the test material between the coupons. The
9、 sandwichedcoupons are cycled between warm ambient air and warmhumid air for 7 days. The coupons are then inspected todetermine whether corrosion more severe than that caused byreagent water has occurred on the surfaces exposed to the testmaterial. This test method is used for solutions of dry granu
10、larmaterial or for liquid materials.5. Significance and Use5.1 The data generated by this test method shall be used todetermine whether aircraft structural aluminum alloys areliable to be corroded or damaged by application of the testmaterial during routine maintenance operations.5.2 Interpretation
11、of the sandwich corrosion test results isbased on a comparison of the appearance of faying surfaces ofthree sets of coupons. One set of test coupons is exposed withreagent water only in the faying surfaces, to establish thebaseline (controls) against which the panels exposed to the testmaterial are
12、compared. Disregard corrosion at cut edges of thetest coupons.5.3 The relative corrosion severity rating system is providedin order to allow a numerical classification of the test resultsand to eliminate the necessity for elaborate weight lossmeasurements. Pitting corrosion, which is rated 4extensiv
13、e(severe) corrosion, may involve only a negligible weight loss.1This test method is under the jurisdiction of ASTM Committee F07 onAerospace and Aircraft and is the direct responsibility of Subcommittee F07.07 onQualification Testing of Aircraft Cleaning Materials.Current edition approved May 1, 200
14、8. Published June 2008. Originallyapproved in 1986. Last previous edition approved in 2002 as F 1110 02.2For referenced ASTM standards, visit the ASTM website, www.astm.org, orcontact ASTM Customer Service at serviceastm.org. For Annual Book of ASTMStandards volume information, refer to the standard
15、s Document Summary page onthe ASTM website.3Available from Society of Automotive Engineers (SAE), 400 CommonwealthDr., Warrendale, PA 15096-0001.4Available from Department of Defense Single Stock Point (DODSSP); http:/dodssp.daps.dla.mil1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C7
16、00, West Conshohocken, PA 19428-2959, United States.5.4 Relative corrosion severity rating system:Appearance/Corrosion:0No visible corrosion and no discoloration present1Very slight corrosion or very slight discoloration, and/or up to 5 % of areaAcorroded2Discoloration and/or up to 10 % of areaAcorr
17、oded3Discoloration and/or up to 25 % of areaAcorroded4Discoloration and/or more than 25 % of areaAcorroded, and/or pittingpresentA”Area” refers to area under the filter paper, or if no filter paper is used, the areawhere the test material was applied.6. Interferences6.1 It is possible that tap water
18、 containing large amounts ofdissolved solids, especially chlorides, will cause relative severecorrosion of the aluminum control panels. For this reason,reagent water is specified. For comparative purposes, a set ofaluminum test panels, with the locally available tap waterapplied to the filter paper,
19、 is sometimes run along with thereagent water panels.6.2 Filter paper made from glass fibers is not recommendedsince, in practice, corrosion of the control panels has often beenfound.7. Apparatus7.1 Humidity Test Cabinet, as specified in Test MethodD 1748 or equal, capable of maintaining 95 to 100 %
20、 relativehumidity at 37.7 6 1C (100 6 2F).7.2 Oven, forced air circulation, capable of maintaining 37.76 1C (100 6 2F).7.3 Microscope, binocular, 103 to 403.8. Reagents and Materials8.1 Purity of WaterUnless otherwise indicated, referencesto water shall be understood to mean reagent water as defined
21、by Specification D 1193, Type IV.8.2 Aluminum Alloy Coupons:8.2.1 Aluminum alloy coupons shall conform to the follow-ing industry standards:SAE-AMS-QQ-A-250/4, 2024-T3 noncladSAE-AMS-QQ-A-250/5, 2024-T3 AlcladSAE-AMS-QQ-A-250/12, 7075-T6 noncladSAE-AMS-QQ-A-250/13, 7075-T6 Alclad8.2.2 Coupon SizeThe
22、 recommended coupon size 50 by100 by 1.0 to 1.5 mm (2 by 4 by 0.04 to 0.06 in.) has beenfound to provide suitable results for comparative tests. Smallersizes are not recommended, because of the increased variationsdue to edge effects. Larger coupons are acceptable, but thespace requirements for test
23、ing and storage shall be taken inconsideration.8.3 Anodize the nonclad coupons in accordance with Mili-tary Specification MIL-A-8625, Type 1 (Chromic Acid) fol-lowed by a hot water seal.8.4 Filter PaperUse Whatman No. 5 or equal filter papermade from cellulose, 11 or 13 cm. Filter paper is not requi
24、redwhen the material being tested is a solid. In case no filter paperis used, the area covered by the test material shall also beapproximately 25 by 75 mm (1 by 3 in.).9. Hazards9.1 The materials used for aircraft maintenance sometimescontain flammable solvents, strong acids or alkalis, or othertoxi
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