ASTM_B_209-14.pdf

B209-14Analysis Aluminum Alloys by the Point to Plane Tech-4.1.8 Tensile property limits and dimensional tolerances fornique Nitrogen Atmosphere(Withdrawn 2011)4sizes not covered in Table 2 or Table 3 of this specification andE716 Practices for Sampling and Sample Preparation ofin ANSI H35.2,respectively.Aluminum and Aluminum Alloys for Determination of4.2 Additionally,orders for material meeting the require-Chemical Composition by Spectrochemical Analysisments of this specification shall include the following infor-E1004 Test Method for Determining Electrical Conductivitymation when required by the purchaser:Using the Electromagnetic(Eddy-Current)Method4.2.1 Whether a supply of one of the pairs of tempers whereE1251 Test Method for Analysis of Aluminum and Alumi-shown in Table 2,(H14 or H24)or(H34 or H24),is specificallynum Alloys by Spark Atomic Emission Spectrometryexcluded(Table 2.Footnote C).G34 Test Method for Exfoliation Corrosion Susceptibility in4.2.2 Whether heat treatment in accordance with Practice2XXX and 7XXX Series Aluminum Alloys(EXCO Test)B918 is required(8.2).G47 Test Method for Determining Susceptibility to Stress-Corrosion Cracking of 2XXX and 7XXX Aluminum4.2.3 Whether solution heat treatment using the hot rollingmill is acceptable(8.3).Alloy Products4.2.4 Whether bend tests are required(12.1).2.3 ANSI Standards:54.2.5 Whether testing for stress-corrosion cracking resis-H35.1/H35.1(M)Alloy and Temper Designation Systems fortance of alloy 2124-T851,2219-T851,or 2219-T87 is requiredAluminum(13.1).H35.2 Dimensional Tolerances for Aluminum Mill Products4.2.6 Whether ultrasonic inspection for aerospace or pres-2.4 AMS Specification:6sure vessels applications is required(Section 17).AMS 2772 Heat Treatment of Aluminum Alloy Raw Mate-4.2.7 Whether inspection or witness of inspection and testsrialsby the purchasers representative is required prior to materialshipment(18.1).2.5 Other Standards:4.2.8 Whether certification is required(Section 22).CEN EN 14242 Aluminum and Aluminum Alloys-4.2.9 Whether there are exceptions to identification markingChemical Analysis-Inductively Coupled Plasma Opticalas provided in B666/B666M(20.1).Emission Spectral Analysis4.2.10 Whether Practices B660 apply and,if so,the levels ofpreservation,packaging,and packing required(21.3).3.Terminology4.2.11 For sheet and plate with tensile properties having3.1 Definitions-Refer to Terminology B881 for definitionsmore than one test direction shown in Table 2 and Table 3,of product terms used in this specification.whether tensile testing should be in a direction other than the3.2 Definitions of Terms Specific to This Standard:direction specified in Test Method B557(Section 9.4).3.2.1 capable ofThe term capable of,as used in this5.Responsibility for Quality Assurancespecification,means that the test need not be performed by theproducer of the material.However,should testing by the5.1 Responsibility for Inspection and Tests-Unless other-purchaser establish that the material does not meet thesewise specified in the contract or purchase order,the producer isrequirements,the material shall be subject to rejectionresponsible for the performance of all inspection and testrequirements specified herein.The producer may use their own4.Ordering Informationor any other suitable facilities for the performance of theinspection and test requirements specified herein,unless dis-4.1 Orders for material to this specification shall include theapproved by the purchaser in the order or at the time of contractfollowing information:signing.The purchaser shall have the right to perform any of4.1.1 This specification designation(which includes thethe inspections and tests set forth in this specification wherenumber,the year,and the revision letter,if applicable).such inspections are deemed necessary to ensure that material4.1.2 Quantity in pieces or pounds.conforms to prescribed requirements.4.1.3Aloy(7.1).4.1.4 Temper(9.1).5.2 Lot Definition-An inspection lot shall be defined as4.1.5 Finish for sheet in nonheat-treatable alloys(Sectionfollows:10).5.2.1 For heat-treated tempers,an inspection lot shall con-4.1.6 For sheet,whether flat or coiled.sist of an identifiable quantity of material of the same mill4.1.7 Dimensions(thickness,width,and length or coil size).form,alloy,temper,and thickness traceable to a heat-treat lotor lots,and subjected to inspection at one time.5.2.2 For nonheat-treated tempers,an inspection lot shallconsist of an identifiable quantity of material of the same mill4The last approved version of this historical standard is referenced onform,alloy,temper,and thickness subjected to inspection atwww.asm.O但s Available from Aluminum Association,Inc.,1525 Wilson Blvd.,Suite 600,one time.Arlington,VA 22209,http:/www.aluminum.org.Available from Society of Automotive Engineers(SAE),400 Commonwealth6.General QualityDr.Warrendale,PA 15096-0001.http:/www.sae.org.7 Available from European Committee for Standardization(CEN),36 Rue de6.1 Unless otherwise specified,the material shall be sup-Stassart,B-1050,Brussels,Belgium,http:/www.cenorm.be.plied in the mill finish,shall be uniform as defined by theB209-14TABLE 1 Chemical Composition Limits4.8.C.MAlloyOther ElementsSiliconIronCopperManganeseMagnesiumChromiumZincTitaniumAluminumEach Total10600.250.350.050.030.030.050.030.03199.60 minG11000.95 Si+Fe0.050.200.05t0.100.050.1599.00 min1230H0.70 Si+Fe0.100.050.050.100.030.0399.30min20140.50-120.73.9-5.00.40-1.20.200.80.100.250.150.050.15remainderAlclad 20142014 clad with 600320240.500.503.8-4.90.30-0.91.2-1.80.100.250.150.050.15remainderAlclad 20242024 clad with 123021240.200.303.84.90.300.91.2-1.80.100.250.150.050.15remainder22190.200.305.86.80.20-0.400.020.100.020.100.050.15remainderAlclad 22192219 clad with 707230030.60.70.050.201.0-1.50.100.050.15remainderAlclad 30033003 clad with 707230040.300.70.251.0-1.50.8-1.30.250.050.15remainderAlclad 30043004 clad with 707230050.60.70.301.0-1.50.20-0.60.100.250.100.050.15remainder31050.60.70.300.30-0.80.200.80.200.400.100.050.15remainder50050.300.70.200.200.50-1.10.100.250.050.15remainder50100.400.70.250.10-0.300.200.60.150.300.100.050.15remainder50500.400.70.200.101.1-1.80.100.250.050.15remainder50520.250.400.100.102.2-2.80.15-0.350.100.050.15remainder50590.450.500.250.6-1.25.0-6.00.250.40-0.90.200.050.15remainder50830.400.400.100.40-1.04.0-4.90.05-0.250.250.150.050.15remainder50860.400.500.100.20-0.73.54.50.05-0.250.250.150.050.15remainder51540.250.400.100.103.1-3.90.15-0.350.200.200.050.15remainder52520.080.100.100.102.2-2.80.050.0340.10remainder52540.45 Si+Fe0.050.013.1-3.90.15-0.350.200.050.050.15remainder54540.250.400.100.50-1.02.4-3.00.05-0.200.250.200.050.15remainder54560.250.400.100.50-1.04.7-5.50.05-0.200.250.200.050.15remainder54570.080.100.200.150.450.8-1.20.050.0310.10remainder56570.080.100.100.030.6-1.00.050.020.05remainder57540.400.400.100.5042.6-3.60.3040.200.150.050.15remainder6003H0.35-1.00.60.100.80.8-1.50.350.200.100.050.15remainder60130.6-1.00.500.6-1.10.200.80.8-1.20.100.250.100.050.15remainder60610.40-0.80.70.150.400.150.8-1.20.04-0.350.250.150.050.15remainderAlclad 60616061 clad with 70727072M0.7 Si+Fe0.100.100.100.8-1.30.050.15remainder70750.400.501.2-2.00.302.1-2.90.18-0.285.1-6.10.200.050.15remainderAlclad 70757075 clad with 7072Limits are in weight percent maximum unless shown as a range or stated otherwise5Analysis shall be made for the elements for which limits are shown in this table.C For purposes of determining conformance to these limits,an observed value or a calculated value attained from analysis shall be rounded to the nearest unit in the lastrighthand place of figures used in expressing the specified limit,in accordance with the Rounding Method of Practice E29.Others includes listed elements for which no specific limit is shown as well as unlisted metallic elements.The producer may analyze samples for trace elements notspecified in the specification.However,such analysis is not required and may not cover all metallic Others elements.Should any analysis by the producer or the purchaserestablish that an Others element exceeds the limit of Each or that the aggregate of several Others elements exceeds the limit of Tofal,the material shall be consideredThe Tota ordooindinthithommitsOther Elements-Total shall be the sum of unspecified metallic elements,0.010%or more,rounded to the second decimal before determining the sum.FVanadium 0.05 maxThe aluminum content shall be calculated by subtracting from 100.00%the sum of all metallic elements present in amounts of 0.010%or more each,rounded to thesecond decimal before determining the sum.Composition of cladding alloy as applied during the course of manufacture.Samples from finished sheet or plate shall not be required to conform to these limits.Vanadium 0.05-0.15,zirconium 0.10-0.250.05-0.25ZrGallium 0.03 max,vanadium 0.05 max.0.10-0.6Mn+Cr.M In case there is a discrepancy in the values listed in Table 2 with those listed in the International Alloy Designations and Chemical Composition Limits for WroughtAluminum and Wrought Aluminum Alloys(known as the Teal Sheets),the composition limits registered with the Aluminum Association and published in the Teal Sheetsshall be considered the controlling composition.The Teal Sheetsare available at http:/www.aluminum.org/tealsheets.requirements of this specification,and shall be commercially7.Chemical Compositionsound.Any requirement not covered is subject to negotiation7.1 Limits-The sheet and plate shall conform to the chemi-between producer and purchaser.cal composition limits specified in Table 1.Conformance shall6.2 Each sheet and plate shall be examined to determinebe determined by the producer by analyzing samples taken atconformance to this specification with respect to generalthe time the ingots are poured in accordance with Practicesquality and identification marking.On approval of theE716 and analyzed in accordance with Test Methods E34,purchaser,however,the producer may use a system of statis-E607,or E1251,or with EN 14242.At least one sample shalltical quality control for such examinations.be taken for each group of ingots poured simultaneously fromB209-14TABLE 2 ContinuedTensile Strength,ksiYield Strength(0.2%offset).ksiElongation inBendSpecified2 in.or 4xDiameterAlloyTemperminmaxminmaxThickness,in.Diameter,Factor,Nmin,%3003H14C or H240.1620.24920.026.017.073003H14C or H240.250-0.49920.026.017.083003H14C or H2400.500-1.00020.026.017.013003H16C or H260.0060.01924.030.021.03003H16C or H26C0.020-0.03124.030.021.03003H16C or H2690.0320.05024.030.0223443003H16C or H2690.051-0.16224.030.021.0463003H18C or H28C0.0060.01927.03003H18C or H2800.0200.0312702823003H18C or H2890.0320.05027.024.03003H18C or H2800.051-0.12827.024.0343003H1120.250-0.49917.0103003H1120.500-2.00015.003003H1122.001-3.00014.5.121830030.250-3.000Alclad 300300.006-0.00713.018.0Alclad 300300.008-0.01213.018.0Alclad 30030.013-0.03113.0104Alclad 30030.0320.05013.0Alclad 3003O0.051-0.24913.018Alclad 30030.250-0.49913.085Alclad 300300.500-3.00014.095.0Alclad 3003H12C or H2200.017-0.03116.00Alclad 3003H12C or H22G0.032-0.05016.022.11Alclad 3003H12C or H22C0.051-0.11316.01.0Alclad 3003H12C or H2200.114-0.16116.0041803533456789Alclad 30030.1620.24916.022011.0Alclad 3003H12C or H2200.250-0.49916.021Alclad 3003H12C or H22c0.500-2.00017.0523.0512.050Alclad 3003H14C or H24C0.009-0.01219.016.0Alclad 3003H14C or H2490.013-0.01919.016.0Alclad 3003H14Cor H24C0.020-0.03119.0216.0Alclad 3003H14C or H240.032-0.05019.0016.0Alclad 3003H14C or H24G0.051-0.11319.012345016.0Alclad 3003H14C or H24C0.114-0.16119.016.0Alclad 3003H14C or H24C0.162-0.24919.020016.067Alclad 3003H14C or H24C0.250-0.49919.025.016.0Alclad 3003H14C or H24C0.500-1.00020.26.0917.0.Alclad 3003H16C or H26c0.0060.01923020.0101Alclad 3003H16C or H2690.020-0.03123.29.20.0Alclad 3003H16C or H2690.032-0.05023.020.0Alclad 30030.051-0.16223.020.0234Alclad 3003H180.006-0.01926.0Alclad 3003H180.020-0.03126.0Alclad 3003H180.0320.05026.0123Alclad 3003H180.051-0.12826.0Alclad 3003H1120.2500.49916.09.048Alclad 3003H1120.500-2.00015.056.09Alclad 3003H1122.001-3.00014.556.0518Alclad 30030.250-3.00030040.0060.00722.029.08.53004000.008-0.01922.029.08130040.020-0.03122.0030040.0320.05022.084163004300480.051-0.24922.00.250-3.00022.08.”181603004H32C or H22C0.017-0.01g28.03521.003004H32C or H22c0.020-0.03128.0813004H32C or H2200.032-0.0502803004H32C or H22C0.051-0.11328.035.2123004H32C or H2200.114-2.00028.035.03004H34C or H24C0.0090.01932.0388023004H34C or H24C0.020-0.05032.025.0134561343004H34C or H2490.051-0.11332.038025.0343004H34Cor H24c0.114-1.00032.0325.03004H36C or H2690.0060.00735.041.028.03004H36C or H2690.0080.01935.041.028.03004H36C or H26c0.0200.03135.041.028.026