ASTM B209/B209M-21a

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:B209/B209M −21a
Standard Specification for
Aluminum and Aluminum-Alloy Sheet and Plate
This standard is issued under the fixed designation B209/B209M; the number immediately following the designation indicates the year
of original adoption or, in the case of revision, the year of last revision.Anumber 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* responsibility of the user of this standard to establish appro-
2 priate safety, health, and environmental practices and deter-
1.1 This specification covers aluminum and aluminum-
mine the applicability of regulatory limitations prior to use.
alloy flat sheet, coiled sheet, and plate in the alloys (Note 1)
1.6 This international standard was developed in accor-
and tempers shown in Tables 2, 3, 4, and 5, and in the
dance with internationally recognized principles on standard-
following finishes:
ization established in the Decision on Principles for the
1.1.1 Plate in all alloys and sheet in heat-treatable alloys:
Development of International Standards, Guides and Recom-
mill finish.
mendations issued by the World Trade Organization Technical
1.1.2 Sheet in nonheat-treatable alloys: mill finish, one-side
Barriers to Trade (TBT) Committee.
bright mill finish, standard one-side bright finish, and standard
two-sides bright finish.
2. Referenced Documents
1.2 Alloy and temper designations are in accordance with
2.1 The following documents of the issue in effect on date
ANSI H35.1/H35.1M. The equivalent Unified Numbering
of material purchase form a part of this specification to the
SystemalloydesignationsarethoseofTable1precededbyA9,
extent referenced herein:
for example, A91100 for aluminum 1100 in accordance with
2.2 ASTM Standards:
Practice E527.
B548Test Method for Ultrasonic Inspection of Aluminum-
NOTE 1—Throughout this specification, use of the term alloy in the
Alloy Plate for Pressure Vessels
general sense includes aluminum as well as aluminum alloy.
B557Test Methods for Tension Testing Wrought and Cast
NOTE 2—See Specification B632/B632M for tread plate.
NOTE 3—See Specification B928/B928M for 5xxx-H116 and 5xxx- Aluminum- and Magnesium-Alloy Products
H321 aluminum alloys containing 3% or more nominal magnesium and
B557MTest Methods forTensionTestingWrought and Cast
intended for marine service and similar environments. Other alloy-temper
Aluminum- and Magnesium-Alloy Products (Metric)
products listed in this specification, which do not require the additional
B594Practice for Ultrasonic Inspection ofAluminum-Alloy
corrosion testing/capability called out in Specification B928/B928M, may
Wrought Products
be suitable for marine and similar environment applications.
B632/B632M Specification for Aluminum-Alloy Rolled
1.3 For acceptance criteria for inclusion of new aluminum
Tread Plate
and aluminum alloys in this specification, see Annex A2.
B660Practices for Packaging/Packing of Aluminum and
1.4 The values stated in either SI units or inch-pound units
Magnesium Products
are to be regarded separately as standard. The values stated in
B666/B666MPractice for Identification Marking of Alumi-
each system are not necessarily exact equivalents; therefore, to
num and Magnesium Products
ensure conformance with the standard, each system shall be
B881Terminology Relating toAluminum- and Magnesium-
used independently of the other, and values from the two
Alloy Products
systems shall not be combined.
B918/B918MPractice for Heat Treatment of Wrought Alu-
1.5 This standard does not purport to address all of the minum Alloys
safety concerns, if any, associated with its use. It is the B928/B928M Specification for High Magnesium
Aluminum-AlloyProductsforMarineServiceandSimilar
Environments
This specification is under the jurisdiction ofASTM Committee B07 on Light
B947Practice for Hot Rolling Mill Solution HeatTreatment
Metals and Alloys and is the direct responsibility of Subcommittee B07.03 on
Aluminum Alloy Wrought Products.
Current edition approved Dec. 1, 2021. Published January 2022. Originally
approved in 1946. Last previous edition approved in 2021 as B209/B209M–21. For referenced ASTM standards, visit the ASTM website, www.astm.org, or
DOI: 10.1520/B0209_B0209M-21A. contact ASTM Customer Service at service@astm.org. For Annual Book of ASTM
For ASME Boiler and Pressure Vessel Code applications see related Specifi- Standards volume information, refer to the standard’s Document Summary page on
cation SB-209 in Section II of that Code. the ASTM website.
*A Summary of Changes section appears at the end of this standard
Copyright © ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States
B209/B209M−21a
for Aluminum Alloy Plate emission spectral analysis
B985Practice for SamplingAluminum Ingots, Billets, Cast-
ings and Finished or Semi-Finished Wrought Aluminum
3. Terminology
Products for Compositional Analysis
3.1 Definitions:
E29Practice for Using Significant Digits in Test Data to
3.1.1 Refer to Terminology B881 for definitions of product
Determine Conformance with Specifications
terms used in this specification.
E34Test Methods for Chemical Analysis of Aluminum and
3.2 Definitions of Terms Specific to This Standard:
Aluminum-Base Alloys (Withdrawn 2017)
3.2.1 capable of—the term capable of, as used in this
E290Test Methods for Bend Testing of Material for Ductil-
specification, means that the test need not be performed by the
ity
producer of the material; however, should testing by the
E527Practice for Numbering Metals and Alloys in the
purchaser establish that the material does not meet these
Unified Numbering System (UNS)
requirements, the material shall be subject to rejection.
E607 Test Method for Atomic Emission Spectrometric
Analysis Aluminum Alloys by the Point to Plane Tech-
4. Ordering Information
nique Nitrogen Atmosphere (Withdrawn 2011)
4.1 Ordersformaterialtothisspecificationshallincludethe
E716Practices for Sampling and Sample Preparation of
following information:
Aluminum and Aluminum Alloys for Determination of
4.1.1 This specification designation (which includes the
Chemical Composition by Spark Atomic Emission Spec-
number, the year, and the revision letter, if applicable).
trometry
4.1.2 Quantity in pieces or pounds.
E1004Test Method for Determining Electrical Conductivity
4.1.3 Alloy (7.1).
Using the Electromagnetic (Eddy Current) Method
E1251Test Method for Analysis of Aluminum and Alumi- 4.1.4 Temper (9.1).
num Alloys by Spark Atomic Emission Spectrometry 4.1.5 Finish for sheet in nonheat-treatable alloys (Section
G34Test Method for Exfoliation Corrosion Susceptibility in 1).
2XXX and 7XXX SeriesAluminumAlloys (EXCO Test) 4.1.6 For sheet, whether flat or coiled.
G47Test Method for Determining Susceptibility to Stress-
4.1.7 Dimensions(thickness,width,andlengthorcoilsize).
Corrosion Cracking of 2XXX and 7XXX Aluminum
4.1.8 Tensile property limits and dimensional tolerances for
Alloy Products
sizesnotcoveredinTable2,Table3,Table4,orTable5ofthis
2.3 ANSI Standards:
specification or in ANSI H35.2 [H35.2M].
H35.1/H35.1MAmericanNationalStandardAlloyandTem-
4.2 Additionally, orders for material meeting the require-
per Designation Systems for Aluminum
ments of this specification shall include the following infor-
H35.2American National Standard Dimensional Tolerances
mation when required by the purchaser:
for Aluminum Mill Products
4.2.1 Whetherasupplyofoneofthepairsoftemperswhere
H35.2MAmerican National Standard Dimensional Toler-
shown in Table 2 or Table 3, (H14 or H24) or (H34 or H24), is
ances for Aluminum Mill Products (Metric)
specifically excluded (Table 2 and Table 3, Footnote C).
2.4 ISO Standards:
4.2.2 Whether heat treatment in accordance with Practice
ISO 209-1Wrought aluminium and aluminium alloys –
B918/B918M is required (8.2).
Chemical composition and forms of products – Part 1:
4.2.3 Whether solution heat treatment using the hot rolling
Chemical composition
mill is acceptable (8.3).
ISO 2107Aluminium and aluminium alloys – Wrought
4.2.4 Whether bend tests are required (12.1).
products – Temper designations
4.2.5 Whether testing for stress-corrosion cracking resis-
ISO 6361-2Wrought aluminium and aluminium alloys –
tance of alloy 2124-T851, 2219-T851, or 2219-T87 is required
Sheets, strips and plates – Part 2: Mechanical properties
7 (13.1).
2.5 AMS Specification:
4.2.6 Whether ultrasonic inspection for aerospace or pres-
AMS2772Heat Treatment ofAluminumAlloy Raw Materi-
sure vessels applications is required (Section 17).
als
4.2.7 Whether inspection or witness of inspection and tests
2.6 CEN Standard:
by the purchaser’s representative is required prior to material
CEN - EN 14242Aluminium and aluminium alloys –
shipment (18.1).
Chemical analysis – Inductively coupled plasma optical
4.2.8 Whether certification is required (Section 22).
4.2.9 Whetherthereareexceptionstoidentificationmarking
The last approved version of this historical standard is referenced on
www.astm.org. as provided in B666/B666M (20.1).
Available fromAluminumAssociation, 1400 Crystal Dr., Suite 430,Arlington,
4.2.10 WhetherPracticesB660applyand,ifso,thelevelsof
VA 22202, http://www.aluminum.org.
preservation, packaging, and packing required (21.3).
Available from International Organization for Standardization (ISO), ISO
4.2.11 For sheet and plate with tensile properties having
Central Secretariat, Chemin de Blandonnet 8, CP 401, 1214 Vernier, Geneva,
Switzerland, https://www.iso.org.
more than one test direction shown in Table 2, Table 3, Table
AvailablefromSAEInternational(SAE),400CommonwealthDr.,Warrendale,
4, and Table 5, whether tensile testing should be in a direction
PA 15096, http://www.sae.org.
other than the direction specified in Test Method B557 or
Available from European Committee for Standardization (CEN), Avenue
Marnix 17, B-1000, Brussels, Belgium, http://www.cen.eu. B557M (Subsection 9.4).
B209/B209M−21a
A,B,C,M
TABLE 1 Chemical Composition Limits
D
Other Elements
Alloy Silicon Iron Copper Manganese Magnesium Chromium Zinc Titanium Aluminum
E
Each Total
F G
1060 0.25 0.35 0.05 0.03 0.03 . 0.05 0.03 0.03 . 99.60 min
G
1100 0.95 Si + Fe 0.05–0.20 0.05 . . 0.10 . 0.05 0.15 99.00 min
G
H F
99.30 min
1230 0.70 Si + Fe 0.10 0.05 0.05 . 0.10 0.03 0.03 .
2014 0.50–1.2 0.7 3.9–5.0 0.40–1.2 0.20–0.8 0.10 0.25 0.15 0.05 0.15 remainder
Alclad 2014 2014 clad with 6003
2024 0.50 0.50 3.8–4.9 0.30–0.9 1.2–1.8 0.10 0.25 0.15 0.05 0.15 remainder
Alclad 2024 2024 clad with 1230
2124 0.20 0.30 3.8–4.9 0.30–0.9 1.2–1.8 0.10 0.25 0.15 0.05 0.15 remainder
I I
2219 0.20 0.30 5.8–6.8 0.20–0.40 0.02 . 0.10 0.02–0.10 0.05 0.15 remainder
Alclad 2219 2219 clad with 7072
3003 0.6 0.7 0.05–0.20 1.0–1.5 . . 0.10 . 0.05 0.15 remainder
Alclad 3003 3003 clad with 7072
3004 0.30 0.7 0.25 1.0–1.5 0.8–1.3 . 0.25 . 0.05 0.15 remainder
Alclad 3004 3004 clad with 7072
3005 0.6 0.7 0.30 1.0–1.5 0.20–0.6 0.10 0.25 0.10 0.05 0.15 remainder
3105 0.6 0.7 0.30 0.30–0.8 0.20–0.8 0.20 0.40 0.10 0.05 0.15 remainder
5005 0.30 0.7 0.20 0.20 0.50–1.1 0.10 0.25 . 0.05 0.15 remainder
5010 0.40 0.7 0.25 0.10–0.30 0.20–0.6 0.15 0.30 0.10 0.05 0.15 remainder
5050 0.40 0.7 0.20 0.10 1.1–1.8 0.10 0.25 . 0.05 0.15 remainder
5052 0.25 0.40 0.10 0.10 2.2–2.8 0.15–0.35 0.10 . 0.05 0.15 remainder
J
5059 0.45 0.50 0.25 0.6–1.2 5.0–6.0 0.25 0.40–0.9 0.20 0.05 0.15 remainder
5083 0.40 0.40 0.10 0.40–1.0 4.0–4.9 0.05–0.25 0.25 0.15 0.05 0.15 remainder
5086 0.40 0.50 0.10 0.20–0.7 3.5–4.5 0.05–0.25 0.25 0.15 0.05 0.15 remainder
5154 0.25 0.40 0.10 0.10 3.1–3.9 0.15–0.35 0.20 0.20 0.05 0.15 remainder
F F
5252 0.08 0.10 0.10 0.10 2.2–2.8 . 0.05 . 0.03 0.10 remainder
5254 0.45 Si + Fe 0.05 0.01 3.1–3.9 0.15–0.35 0.20 0.05 0.05 0.15 remainder
5454 0.25 0.40 0.10 0.50–1.0 2.4–3.0 0.05–0.20 0.25 0.20 0.05 0.15 remainder
5456 0.25 0.40 0.10 0.50–1.0 4.7–5.5 0.05–0.20 0.25 0.20 0.05 0.15 remainder
F F
5457 0.08 0.10 0.20 0.15–0.45 0.8–1.2 . 0.05 . 0.03 0.10 remainder
K K
5657 0.08 0.10 0.10 0.03 0.6–1.0 . 0.05 . 0.02 0.05 remainder
L L
5754 0.40 0.40 0.10 0.50 2.6-3.6 0.30 0.20 0.15 0.05 0.15 remainder
H
6003 0.35–1.0 0.6 0.10 0.8 0.8–1.5 0.35 0.20 0.10 0.05 0.15 remainder
6013 0.6–1.0 0.50 0.6–1.1 0.20–0.8 0.8–1.2 0.10 0.25 0.10 0.05 0.15 remainder
6061 0.40–0.8 0.7 0.15–0.40 0.15 0.8–1.2 0.04–0.35 0.25 0.15 0.05 0.15 remainder
Alclad 6061 6061 clad with 7072
H
7072 0.7 Si + Fe 0.10 0.10 0.10 . 0.8–1.3 . 0.05 0.15 remainder
7075 0.40 0.50 1.2–2.0 0.30 2.1–2.9 0.18–0.28 5.1–6.1 0.20 0.05 0.15 remainder
Alclad 7075 7075 clad with 7072
A
Limits are in weight percent maximum unless shown as a range or stated otherwise.
B
Analysis 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 last
righthand place of figures used in expressing the specified limit, in accordance with the Rounding Method of Practice E29.
D
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 not
specified in the specification. However, such analysis is not required and may not cover all metallicOthers elements. Should any analysis by the producer or the purchaser
establish that an Others element exceeds the limit of Each or that the aggregate of several Others elements exceeds the limit of Total, the material shall be considered
nonconforming. The Total for Other Elements does not include elements shown in the footnotes with specific composition limits.
E
Other Elements—Total shall be the sum of unspecified metallic elements, 0.010 % or more, rounded to the second decimal before determining the sum.
F
Vanadium 0.05 max.
G
The 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, roundedtothe
second decimal before determining the sum.
H
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.
I
Vanadium 0.05–0.15, zirconium 0.10–0.25.
J
0.05–0.25 Zr
K
Gallium 0.03 max, vanadium 0.05 max.
L
0.10–0.6 Mn + Cr.
M
In case there is a discrepancy in the values listed in Table 1 with those listed in the “International Alloy Designations and Chemical Composition Limits for Wrought
Aluminum and Wrought Aluminum Alloys” (known as the “Teal Sheets”), the composition limits registered with the Aluminum Association and published in the “Teal Sheets”
shall be considered the controlling composition. The “Teal Sheets” are available at http://www.aluminum.org/tealsheets.
5. Responsibility for Quality Assurance the inspections and tests set forth in this specification where
such inspections are deemed necessary to ensure that material
5.1 Responsibility for Inspection and Tests—Unless other-
conforms to prescribed requirements.
wisespecifiedinthecontractorpurchaseorder,theproduceris
responsible for the performance of all inspection and test 5.2 Lot Definition—An inspection lot shall be defined as
requirementsspecifiedherein.Theproducermayusetheirown follows:
or any other suitable facilities for the performance of the 5.2.1 For heat-treated tempers, an inspection lot shall con-
inspection and test requirements specified herein, unless dis- sist of an identifiable quantity of material of the same mill
approvedbythepurchaserintheorderoratthetimeofcontract form, alloy, temper, and thickness traceable to a heat-treat lot
signing. The purchaser shall have the right to perform any of or lots, and subjected to inspection at one time.
B209/B209M−21a
A,B,G
TABLE 2 Mechanical Property Limits for Nonheat-treatable Alloy, Inch-Pound Units
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
Factor, N
min max min max
min, %
1060 O 0.006–0.019 8.0 14.0 2.5 . 15 .
1060 O 0.020–0.050 8.0 14.0 2.5 . 22 .
1060 O 0.051–3.000 8.0 14.0 2.5 . 25 .
C C
1060 H12 or H22 0.017–0.050 11.0 16.0 9.0 . 6 .
C C
1060 H12 or H22 0.051–2.000 11.0 16.0 9.0 . 12 .
C C
1060 H14 or H24 0.009–0.019 12.0 17.0 10.0 . 1 .
C C
1060 H14 or H24 0.020–0.050 12.0 17.0 10.0 . 5 .
C C
1060 H14 or H24 0.051–1.000 12.0 17.0 10.0 . 10 .
C C
1060 H16 or H26 0.006–0.019 14.0 19.0 11.0 . 1 .
C C
1060 H16 or H26 0.020–0.050 14.0 19.0 11.0 . 4 .
C C
1060 H16 or H26 0.051–0.162 14.0 19.0 11.0 . 5 .
C C
1060 H18 or H28 0.006–0.019 16.0 . 12.0 . 1 .
C C
1060 H18 or H28 0.020–0.050 16.0 . 12.0 . 3 .
C C
1060 H18 or H28 0.051–0.128 16.0 . 12.0 . 4 .
1060 H112 0.250–0.499 11.0 . 7.0 . 10 .
1060 H112 0.500–1.000 10.0 . 5.0 . 20 .
1060 H112 1.001–3.000 9.0 . 4.0 . 25 .
1060 F 0.250–3.000 . . . . . .
1100 O 0.006–0.019 11.0 15.5 3.5 . 15 0
1100 O 0.020–0.031 11.0 15.5 3.5 . 20 0
1100 O 0.032–0.050 11.0 15.5 3.5 . 25 0
1100 O 0.051–0.249 11.0 15.5 3.5 . 30 0
1100 O 0.250–3.000 11.0 15.5 3.5 . 28 0
C C
1100 H12 or H22 0.017–0.019 14.0 19.0 11.0 . 3 0
C C
1100 H12 or H22 0.020–0.031 14.0 19.0 11.0 . 4 0
C C
1100 H12 or H22 0.032–0.050 14.0 19.0 11.0 . 6 0
C C
1100 H12 or H22 0.051–0.113 14.0 19.0 11.0 . 8 0
C C
1100 H12 or H22 0.114–0.499 14.0 19.0 11.0 . 9 0
C C
1100 H12 or H22 0.500–2.000 14.0 19.0 11.0 . 12 0
C C
1100 H14 or H24 0.009–0.012 16.0 21.0 14.0 . 1 0
C C
1100 H14 or H24 0.013–0.019 16.0 21.0 14.0 . 2 0
C C
1100 H14 or H24 0.020–0.031 16.0 21.0 14.0 . 3 0
C C
1100 H14 or H24 0.032–0.050 16.0 21.0 14.0 . 4 0
C C
1100 H14 or H24 0.051–0.113 16.0 21.0 14.0 . 5 0
C C
1100 H14 or H24 0.114–0.499 16.0 21.0 14.0 . 6 0
C C
1100 H14 or H24 0.500–1.000 16.0 21.0 14.0 . 10 0
C C
1100 H16 or H26 0.006–0.019 19.0 24.0 17.0 . 1 4
C C
1100 H16 or H26 0.020–0.031 19.0 24.0 17.0 . 2 4
C C
1100 H16 or H26 0.032–0.050 19.0 24.0 17.0 . 3 4
C C
1100 H16 or H26 0.051–0.162 19.0 24.0 17.0 . 4 4
C C
1100 H18 or H28 0.006–0.019 22.0 . . . 1 .
C C
1100 H18 or H28 0.020–0.031 22.0 . . . 2 .
C C
1100 H18 or H28 0.032–0.050 22.0 . . . 3 .
C C
1100 H18 or H28 0.051–0.128 22.0 . . . 4 .
1100 H112 0.250–0.499 13.0 7.0 . 9 .
1100 H112 0.500–2.000 12.0 . 5.0 . 14 .
1100 H112 2.001–3.000 11.5 . 4.0 . 20 .
D
1100 F 0.250–3.000 . . . . . .
3003 O 0.006–0.007 14.0 19.0 5.0 . 14 0
3003 O 0.008–0.012 14.0 19.0 5.0 . 18 0
3003 O 0.013–0.031 14.0 19.0 5.0 . 20 0
3003 O 0.032–0.050 14.0 19.0 5.0 . 23 0
3003 O 0.051–0.249 14.0 19.0 5.0 . 25 0
3003 O 0.250–3.000 14.0 19.0 5.0 . 23 .
C C
3003 H12 or H22 0.017–0.019 17.0 23.0 12.0 . 3 0
C C
3003 H12 or H22 0.020–0.031 17.0 23.0 12.0 . 4 0
C C
3003 H12 or H22 0.032–0.050 17.0 23.0 12.0 . 5 0
C C
3003 H12 or H22 0.051–0.113 17.0 23.0 12.0 . 6 0
C C
3003 H12 or H22 0.114–0.161 17.0 23.0 12.0 . 7 0
C C
3003 H12 or H22 0.162–0.249 17.0 23.0 12.0 . 8 0
C C
3003 H12 or H22 0.250–0.499 17.0 23.0 12.0 . 9 .
C C
3003 H12 or H22 0.500–2.000 17.0 23.0 12.0 . 10 .
C C
3003 H14 or H24 0.009–0.012 20.0 26.0 17.0 . 1 0
C C
3003 H14 or H24 0.013–0.019 20.0 26.0 17.0 . 2 0
C C
3003 H14 or H24 0.020–0.031 20.0 26.0 17.0 . 3 0
C C
3003 H14 or H24 0.032–0.050 20.0 26.0 17.0 . 4 0
C C
3003 H14 or H24 0.051–0.113 20.0 26.0 17.0 . 5 0
C C
3003 H14 or H24 0.114–0.161 20.0 26.0 17.0 . 6 2
B209/B209M−21a
TABLE2 Continued
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi
Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
min max min max Factor, N
min, %
C C
3003 H14 or H24 0.162–0.249 20.0 26.0 17.0 . 7 2
C C
3003 H14 or H24 0.250–0.499 20.0 26.0 17.0 . 8 .
C C
3003 H14 or H24 0.500–1.000 20.0 26.0 17.0 . 10 .
C C
3003 H16 or H26 0.006–0.019 24.0 30.0 21.0 . 1 4
C C
3003 H16 or H26 0.020–0.031 24.0 30.0 21.0 . 2 4
C C
3003 H16 or H26 0.032–0.050 24.0 30.0 21.0 . 3 4
C C
3003 H16 or H26 0.051–0.162 24.0 30.0 21.0 . 4 6
C C
3003 H18 or H28 0.006–0.019 27.0 . 24.0 . 1 .
C C
3003 H18 or H28 0.020–0.031 27.0 . 24.0 . 2 .
C C
3003 H18 or H28 0.032–0.050 27.0 . 24.0 . 3 .
C C
3003 H18 or H28 0.051–0.128 27.0 . 24.0 . 4 .
3003 H112 0.250–0.499 17.0 . 10.0 . 8 .
3003 H112 0.500–2.000 15.0 . 6.0 . 12 .
3003 H112 2.001–3.000 14.5 . 6.0 . 18 .
D
3003 F 0.250–3.000 . . . . . .
Alclad 3003 O 0.006–0.007 13.0 18.0 4.5 . 14 .
Alclad 3003 O 0.008–0.012 13.0 18.0 4.5 . 18 .
Alclad 3003 O 0.013–0.031 13.0 18.0 4.5 . 20 .
Alclad 3003 O 0.032–0.050 13.0 18.0 4.5 . 23 .
Alclad 3003 O 0.051–0.249 13.0 18.0 4.5 . 25 .
Alclad 3003 O 0.250–0.499 13.0 18.0 4.5 . 23 .
E E E
Alclad 3003 O 0.500–3.000 14.0 19.0 5.0 . 23 .
C C
Alclad 3003 H12 or H22 0.017–0.031 16.0 22.0 11.0 . 4 .
C C
Alclad 3003 H12 or H22 0.032–0.050 16.0 22.0 11.0 . 5 .
C C
Alclad 3003 H12 or H22 0.051–0.113 16.0 22.0 11.0 . 6 .
C C
Alclad 3003 H12 or H22 0.114–0.161 16.0 22.0 11.0 . 7 .
C C
Alclad 3003 H12 or H22 0.162–0.249 16.0 22.0 11.0 . 8 .
C C
Alclad 3003 H12 or H22 0.250–0.499 16.0 22.0 11.0 . 9 .
C C E E E
Alclad 3003 H12 or H22 0.500–2.000 17.0 23.0 12.0 . 10 .
C C
Alclad 3003 H14 or H24 0.009–0.012 19.0 25.0 16.0 . 1 .
C C
Alclad 3003 H14 or H24 0.013–0.019 19.0 25.0 16.0 . 2 .
C C
Alclad 3003 H14 or H24 0.020–0.031 19.0 25.0 16.0 . 3 .
C C
Alclad 3003 H14 or H24 0.032–0.050 19.0 25.0 16.0 . 4 .
C C
Alclad 3003 H14 or H24 0.051–0.113 19.0 25.0 16.0 . 5 .
C C
Alclad 3003 H14 or H24 0.114–0.161 19.0 25.0 16.0 . 6 .
C C
Alclad 3003 H14 or H24 0.162–0.249 19.0 25.0 16.0 . 7 .
C C
Alclad 3003 H14 or H24 0.250–0.499 19.0 25.0 16.0 . 8 .
C C E E E
Alclad 3003 H14 or H24 0.500–1.000 20.0 26.0 17.0 . 10 .
C C
Alclad 3003 H16 or H26 0.006–0.019 23.0 29.0 20.0 . 1 .
C C
Alclad 3003 H16 or H26 0.020–0.031 23.0 29.0 20.0 . 2 .
C C
Alclad 3003 H16 or H26 0.032–0.050 23.0 29.0 20.0 . 3 .
C C
Alclad 3003 H16 or H26 0.051–0.162 23.0 29.0 20.0 . 4 .
Alclad 3003 H18 0.006–0.019 26.0 . . . 1 .
Alclad 3003 H18 0.020–0.031 26.0 . . . 2 .
Alclad 3003 H18 0.032–0.050 26.0 . . . 3 .
Alclad 3003 H18 0.051–0.128 26.0 . . . 4 .
Alclad 3003 H112 0.250–0.499 16.0 . 9.0 . 8 .
E E
Alclad 3003 H112 0.500–2.000 15.0 . 6.0 . 12 .
E E
Alclad 3003 H112 2.001–3.000 14.5 . 6.0 . 18 .
D
Alclad 3003 F 0.250–3.000 . . . . . .
3004 O 0.006–0.007 22.0 29.0 8.5 . . .
3004 O 0.008– 0.019 22.0 29.0 8.5 . 10 0
3004 O 0.020–0.031 22.0 29.0 8.5 . 14 0
3004 O 0.032–0.050 22.0 29.0 8.5 . 16 0
3004 O 0.051–0.249 22.0 29.0 8.5 . 18 0
3004 O 0.250–3.000 22.0 29.0 8.5 . 16 .
C C
3004 H32 or H22 0.017–0.019 28.0 35.0 21.0 . 1 0
C C
3004 H32 or H22 0.020–0.031 28.0 35.0 21.0 . 3 1
C C
3004 H32 or H22 0.032–0.050 28.0 35.0 21.0 . 4 1
C C
3004 H32 or H22 0.051–0.113 28.0 35.0 21.0 . 5 2
C C
3004 H32 or H22 0.114–2.000 28.0 35.0 21.0 . 6 .
C C
3004 H34 or H24 0.009–0.019 32.0 38.0 25.0 . 1 2
C C
3004 H34 or H24 0.020–0.050 32.0 38.0 25.0 . 3 3
C C
3004 H34 or H24 0.051–0.113 32.0 38.0 25.0 . 4 4
C C
3004 H34 or H24 0.114–1.000 32.0 38.0 25.0 . 5 .
C C
3004 H36 or H26 0.006–0.007 35.0 41.0 28.0 . . .
C C
3004 H36 or H26 0.008–0.019 35.0 41.0 28.0 . 1 6
C C
3004 H36 or H26 0.020–0.031 35.0 41.0 28.0 . 2 6
B209/B209M−21a
TABLE2 Continued
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi
Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
min max min max Factor, N
min, %
C C
3004 H36 or H26 0.032–0.050 35.0 41.0 28.0 . 3 6
C C
3004 H36 or H26 0.051–0.162 35.0 41.0 28.0 . 4 8
C C
3004 H38 or H28 0.006–0.007 38.0 . 31.0 . . .
C C
3004 H38 or H28 0.008–0.019 38.0 . 31.0 . 1 .
C C
3004 H38 or H28 0.020–0.031 38.0 . 31.0 . 2 .
C C
3004 H38 or H28 0.032–0.050 38.0 . 31.0 . 3 .
C C
3004 H38 or H28 0.051–0.128 38.0 . 31.0 . 4 .
3004 H112 0.250–3.000 23.0 . 9.0 . 7 .
D
3004 F 0.250–3.000 . . . . . .
Alclad 3004 O 0.006–0.007 21.0 28.0 8.0 . . .
Alclad 3004 O 0.008–0.019 21.0 28.0 8.0 . 10 .
Alclad 3004 O 0.020–0.031 21.0 28.0 8.0 . 14 .
Alclad 3004 O 0.032–0.050 21.0 28.0 8.0 . 16 .
Alclad 3004 O 0.051–0.249 21.0 28.0 8.0 . 18 .
Alclad 3004 O 0.250–0.499 21.0 28.0 8.0 . 16 .
E E E
Alclad 3004 O 0.500–3.000 22.0 29.0 8.5 . 16 .
C C
Alclad 3004 H32 or H22 0.017–0.019 27.0 34.0 20.0 . 1 .
C C
Alclad 3004 H32 or H22 0.020–0.031 27.0 34.0 20.0 . 3 .
C C
Alclad 3004 H32 or H22 0.032–0.050 27.0 34.0 20.0 . 4 .
C C
Alclad 3004 H32 or H22 0.051–0.113 27.0 34.0 20.0 . 5 .
C C
Alclad 3004 H32 or H22 0.114–0.249 27.0 34.0 20.0 . 6 .
C C
Alclad 3004 H32 or H22 0.250–0.499 27.0 34.0 20.0 . 6 .
C C E E E
Alclad 3004 H32 or H22 0.500–2.000 28.0 35.0 21.0 . 6 .
C C
Alclad 3004 H34 or H24 0.009–0.019 31.0 37.0 24.0 . 1 .
C C
Alclad 3004 H34 or H24 0.020–0.050 31.0 37.0 24.0 . 3 .
C C
Alclad 3004 H34 or H24 0.051–0.113 31.0 37.0 24.0 . 4 .
C C
Alclad 3004 H34 or H24 0.114–0.249 31.0 37.0 24.0 . 5 .
C C
Alclad 3004 H34 or H24 0.250–0.499 31.0 37.0 24.0 . 5 .
C C E E E
Alclad 3004 H34 or H24 0.500–1.000 32.0 38.0 25.0 . 5 .
C C
Alclad 3004 H36 or H26 0.006–0.007 34.0 40.0 27.0 . . .
C C
Alclad 3004 H36 or H26 0.008–0.019 34.0 40.0 27.0 . 1 .
C C
Alclad 3004 H36 or H26 0.020–0.031 34.0 40.0 27.0 . 2 .
C C
Alclad 3004 H36 or H26 0.032–0.050 34.0 40.0 27.0 . 3 .
C C
Alclad 3004 H36 or H26 0.051–0.162 34.0 40.0 27.0 . 4 .
Alclad 3004 H38 0.006–0.007 37.0 . . . . .
Alclad 3004 H38 0.008–0.019 37.0 . . . 1 .
Alclad 3004 H38 0.020–0.031 37.0 . . . 2 .
Alclad 3004 H38 0.032–0.050 37.0 . . . 3 .
Alclad 3004 H38 0.051–0.128 37.0 . . . 4 .
Alclad 3004 H112 0.250–0.499 22.0 . 8.5 . 7 .
E E
Alclad 3004 H112 0.500–3.000 23.0 . 9.0 . 7 .
D
Alclad 3004 F 0.250–3.000 . . . . . .
3005 O 0.006–0.007 17.0 24.0 6.5 . 10 .
3005 O 0.008–0.012 17.0 24.0 6.5 . 12 .
3005 O 0.013–0.019 17.0 24.0 6.5 . 14 .
3005 O 0.020–0.031 17.0 24.0 6.5 . 16 .
3005 O 0.032–0.050 17.0 24.0 6.5 . 18 .
3005 O 0.051–0.249 17.0 24.0 6.5 . 20 .
3005 H12 0.017–0.019 20.0 27.0 17.0 . 1 .
3005 H12 0.020–0.050 20.0 27.0 17.0 . 2 .
3005 H12 0.051–0.113 20.0 27.0 17.0 . 3 .
3005 H12 0.114–0.161 20.0 27.0 17.0 . 4 .
3005 H12 0.162–0.249 20.0 27.0 17.0 . 5 .
3005 H14 0.009–0.031 24.0 31.0 21.0 . 1 .
3005 H14 0.032–0.050 24.0 31.0 21.0 . 2 .
3005 H14 0.051–0.113 24.0 31.0 21.0 . 3 .
3005 H14 0.114–0.249 24.0 31.0 21.0 . 4 .
3005 H16 0.006–0.031 28.0 35.0 25.0 . 1 .
3005 H16 0.032–0.113 28.0 35.0 25.0 . 2 .
3005 H16 0.114–0.162 28.0 35.0 25.0 . 3 .
3005 H18 0.006–0.031 32.0 . 29.0 . 1 .
3005 H18 0.032–0.128 32.0 . 29.0 . 2 .
3005 H19 0.006–0.012 34.0 . . . . .
3005 H19 0.013–0.063 34.0 . . . 1 .
3005 H25 0.016–0.019 26.0 34.0 22.0 . 1 .
3005 H25 0.020–0.031 26.0 34.0 22.0 . 2 .
3005 H25 0.032–0.050 26.0 34.0 22.0 . 3 .
3005 H25 0.051–0.080 26.0 34.0 22.0 . 4 .
B209/B209M−21a
TABLE2 Continued
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi
Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
min max min max Factor, N
min, %
3005 H27 0.016–0.019 29.5 37.5 25.5 . 1 .
3005 H27 0.020–0.031 29.5 37.5 25.5 . 2 .
3005 H27 0.032–0.050 29.5 37.5 25.5 . 3 .
3005 H27 0.051–0.080 29.5 37.5 25.5 . 4 .
3005 H28 0.016–0.019 31.0 . 27.0 . 1 .
3005 H28 0.020–0.031 31.0 . 27.0 . 2 .
3005 H28 0.032–0.050 31.0 . 27.0 . 3 .
3005 H28 0.051–0.080 31.0 . 27.0 . 4 .
3105 O 0.013–0.019 14.0 21.0 5.0 . 16 .
3105 O 0.020–0.031 14.0 21.0 5.0 . 18 .
3105 O 0.032–0.080 14.0 21.0 5.0 . 20 .
3105 H12 0.017–0.019 19.0 26.0 15.0 . 1 .
3105 H12 0.020–0.031 19.0 26.0 15.0 . 1 .
3105 H12 0.032–0.050 19.0 26.0 15.0 . 2 .
3105 H12 0.051–0.080 19.0 26.0 15.0 . 3 .
3105 H14 0.013–0.019 22.0 29.0 18.0 . 1 .
3105 H14 0.020–0.031 22.0 29.0 18.0 . 1 .
3105 H14 0.032–0.050 22.0 29.0 18.0 . 2 .
3105 H14 0.051–0.080 22.0 29.0 18.0 . 2 .
3105 H16 0.013–0.031 25.0 32.0 21.0 . 1 .
3105 H16 0.032–0.050 25.0 32.0 21.0 . 2 .
3105 H16 0.051–0.080 25.0 32.0 21.0 . 2 .
3105 H18 0.013–0.031 28.0 . 24.0 . 1 .
3105 H18 0.032–0.050 28.0 . 24.0 . 1 .
3105 H18 0.051–0.080 28.0 ,,, 24.0 . 2 .
3105 H22 0.013–0.019 19.0 . 15.0 . 3 .
3105 H22 0.020–0.031 19.0 . 15.0 . 4 .
3105 H22 0.032–0.050 19.0 . 15.0 . 5 .
3105 H22 0.051–0.080 19.0 . 15.0 . 6 .
3105 H24 0.013–0.019 22.0 . 18.0 . 2 .
3105 H24 0.020–0.031 22.0 . 18.0 . 3 .
3105 H24 0.032–0.050 22.0 . 18.0 . 4 .
3105 H24 0.051–0.080 22.0 . 18.0 . 6 .
3105 H25 0.013–0.019 23.0 . 19.0 . 2 .
3105 H25 0.020–0.031 23.0 . 19.0 . 3 .
3105 H25 0.032–0.050 23.0 . 19.0 . 4 .
3105 H25 0.051–0.080 23.0 . 19.0 . 6 .
3105 H26 0.013–0.031 25.0 . 21.0 . 3 .
3105 H26 0.032–0.050 25.0 . 21.0 . 4 .
3105 H26 0.051–0.080 25.0 . 21.0 . 5 .
3105 H28 0.013–0.031 28.0 . 24.0 . 2 .
3105 H28 0.032–0.050 28.0 . 24.0 . 3 .
3105 H28 0.051–0.080 28.0 . 24.0 . 4 .
5005 O 0.006–0.007 15.0 21.0 5.0 . 12 .
5005 O 0.008–0.012 15.0 21.0 5.0 . 14 .
5005 O 0.013–0.019 15.0 21.0 5.0 . 16 .
5005 O 0.020–0.031 15.0 21.0 5.0 . 18 .
5005 O 0.032–0.050 15.0 21.0 5.0 . 20 .
5005 O 0.051–0.113 15.0 21.0 5.0 . 21 .
5005 O 0.114–0.249 15.0 21.0 5.0 . 22 .
5005 O 0.250–3.000 15.0 21.0 5.0 . 22 .
5005 H12 0.017–0.019 18.0 24.0 14.0 . 2 .
5005 H12 0.020–0.031 18.0 24.0 14.0 . 3 .
5005 H12 0.032–0.050 18.0 24.0 14.0 . 4 .
5005 H12 0.051–0.113 18.0 24.0 14.0 . 6 .
5005 H12 0.114–0.161 18.0 24.0 14.0 . 7 .
5005 H12 0.162–0.249 18.0 24.0 14.0 . 8 .
5005 H12 0.250–0.499 18.0 24.0 14.0 . 9 .
5005 H12 0.500–2.000 18.0 24.0 14.0 . 10 .
5005 H14 0.009–0.031 21.0 27.0 17.0 . 1 .
5005 H14 0.032–0.050 21.0 27.0 17.0 . 2 .
5005 H14 0.051–0.113 21.0 27.0 17.0 . 3 .
5005 H14 0.114–0.161 21.0 27.0 17.0 . 5 .
5005 H14 0.162–0.249 21.0 27.0 17.0 . 6 .
5005 H14 0.250–0.499 21.0 27.0 17.0 . 8 .
5005 H14 0.500–1.000 21.0 27.0 17.0 . 10 .
5005 H16 0.006–0.031 24.0 30.0 20.0 . 1 .
5005 H16 0.032–0.050 24.0 30.0 20.0 . 2 .
B209/B209M−21a
TABLE2 Continued
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi
Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
min max min max Factor, N
min, %
5005 H16 0.051–0.162 24.0 30.0 20.0 . 3 .
5005 H18 0.006–0.031 27.0 . . . 1 .
5005 H18 0.032–0.050 27.0 . . . 2 .
5005 H18 0.051–0.128 27.0 . . . 3 .
C C
5005 H32 or H22 0.017–0.019 17.0 23.0 12.0 . 3 .
C C
5005 H32 or H22 0.020–0.031 17.0 23.0 12.0 . 4 .
C C
5005 H32 or H22 0.032–0.050 17.0 23.0 12.0 . 5 .
C C
5005 H32 or H22 0.051–0.113 17.0 23.0 12.0 . 7 .
C C
5005 H32 or H22 0.114–0.161 17.0 23.0 12.0 . 8 .
C C
5005 H32 or H22 0.162–0.249 17.0 23.0 12.0 . 9 .
C C
5005 H32 or H22 0.250–2.000 17.0 23.0 12.0 . 10 .
C C
5005 H34 or H24 0.009–0.012 20.0 26.0 15.0 . 2 .
C C
5005 H34 or H24 0.013–0.031 20.0 26.0 15.0 . 3 .
C C
5005 H34 or H24 0.032–0.050 20.0 26.0 15.0 . 4 .
C C
5005 H34 or H24 0.051–0.113 20.0 26.0 15.0 . 5 .
C C
5005 H34 or H24 0.114–0.161 20.0 26.0 15.0 . 6 .
C C
5005 H34 or H24 0.162–0.249 20.0 26.0 15.0 . 7 .
C C
5005 H34 or H24 0.250–0.499 20.0 26.0 15.0 . 8 .
C C
5005 H34 or H24 0.500–1.000 20.0 26.0 15.0 . 10 .
C C
5005 H36 or H26 0.006–0.007 23.0 29.0 18.0 . 1 .
C C
5005 H36 or H26 0.008–0.019 23.0 29.0 18.0 . 2 .
C C
5005 H36 or H26 0.020–0.031 23.0 29.0 18.0 . 3 .
C C
5005 H36 or H26 0.032–0.162 23.0 29.0 18.0 . 4 .
5005 H38 0.006–0.012 26.0 . . . 1 .
5005 H38 0.013–0.019 26.0 . . . 2 .
5005 H38 0.020–0.031 26.0 . . . 3 .
5005 H38 0.032–0.128 26.0 . . . 4 .
5005 H112 0.250–0.499 17.0 . . . 8 .
5005 H112 0.500–2.000 15.0 . . . 12 .
5005 H112 2.001–3.000 14.5 . . . 18 .
D
5005 F 0.250–3.000 . . . . . .
5010 O 0.010–0.070 15.0 21.0 5.0 . 3 .
5010 H22 0.010–0.070 17.0 23.0 14.0 . 2 .
5010 H24 0.010–0.070 20.0 26.0 17.0 . 1 .
5010 H26 0.010–0.070 23.0 29.0 21.0 . 1 .
5010 H28 0.010–0.070 26.0 . . . . .
5050 O 0.006–0.007 18.0 24.0 6.0 . . 0
5050 O 0.008–0.019 18.0 24.0 6.0 . 16 0
5050 O 0.020–0.031 18.0 24.0 6.0 . 18 0
5050 O 0.032–0.113 18.0 24.0 6.0 . 20 0
5050 O 0.114–0.249 18.0 24.0 6.0 . 22 0
5050 O 0.250–3.000 18.0 24.0 6.0 . 20 2
C C
5050 H32 or H22 0.017–0.050 22.0 28.0 16.0 . 4 1
C C
5050 H32 or H22 0.051–0.249 22.0 28.0 16.0 . 6 2
C C
5050 H34 or H24 0.009–0.031 25.0 31.0 20.0 . 3 1
C C
5050 H34 or H24 0.032–0.050 25.0 31.0 20.0 . 4 1
C C
5050 H34 or H24 0.051–0.249 25.0 31.0 20.0 . 5 3
C C
5050 H36 or H26 0.006–0.019 27.0 33.0 22.0 . 2 3
C C
5050 H36 or H26 0.020–0.050 27.0 33.0 22.0 . 3 3
C C
5050 H36 or H26 0.051–0.162 27.0 33.0 22.0 . 4 4
5050 H38 0.006–0.007 29.0 . . . . .
5050 H38 0.008–0.031 29.0 . . . 2 .
5050 H38 0.032–0.050 29.0 . . . 3 .
5050 H38 0.051–0.128 29.0 . . . 4 .
5050 H112 0.250–3.000 20.0 . 8.0 . 12 .
D
5050 F 0.250–3.000 . . . . . .
5052 O 0.006–0.007 25.0 31.0 9.5 . . 0
5052 O 0.008–0.012 25.0 31.0 9.5 . 14 0
5052 O 0.013–0.019 25.0 31.0 9.5 . 15 0
5052 O 0.020–0.031 25.0 31.0 9.5 . 16 0
5052 O 0.032–0.050 25.0 31.0 9.5 . 18 0
5052 O 0.051–0.113 25.0 31.0 9.5 . 19 0
5052 O 0.114–0.249 25.0 31.0 9.5 . 20 0
5052 O 0.250–3.000 25.0 31.0 9.5 . 18 .
5052 H141 0.090-0.174 35.5 . 24.0 . 6 .
5052 H141 0.175-0.300 34.0 . 24.0 . 8 .
B209/B209M−21a
TABLE2 Continued
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi
Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
min max min max Factor, N
min, %
C C
5052 H32 or H22 0.017–0.019 31.0 38.0 23.0 . 4 0
C C
5052 H32 or H22 0.020–0.050 31.0 38.0 23.0 . 5 1
C C
5052 H32 or H22 0.051–0.113 31.0 38.0 23.0 . 7 2
C C
5052 H32 or H22 0.114–0.249 31.0 38.0 23.0 . 9 3
C C
5052 H32 or H22 0.250–0.499 31.0 38.0 23.0 . 11 .
C C
5052 H32 or H22 0.500–2.000 31.0 38.0 23.0 . 12 .
C C
5052 H34 or H24 0.009–0.019 34.0 41.0 26.0 . 3 1
C C
5052 H34 or H24 0.020–0.050 34.0 41.0 26.0 . 4 2
C C
5052 H34 or H24 0.051–0.113 34.0 41.0 26.0 . 6 3
C C
5052 H34 or H24 0.114–0.249 34.0 41.0 26.0 . 7 4
C C
5052 H34 or H24 0.250–1.000 34.0 41.0 26.0 . 10 .
C C
5052 H36 or H26 0.006–0.007 37.0 44.0 29.0 . 2 4
C C
5052 H36 or H26 0.008–0.031 37.0 44.0 29.0 . 3 4
C C
5052 H36 or H26 0.032–0.162 37.0 44.0 29.0 . 4 5
C C
5052 H38 or H28 0.006–0.007 39.0 . 32.0 . 2 .
C C
5052 H38 or H28 0.008–0.031 39.0 . 32.0 . 3 .
C C
5052 H38 or H28 0.032–0.128 39.0 . 32.0 . 4 .
5052 H112 0.250–0.499 28.0 . 16.0 . 7 .
5052 H112 0.500–2.000 25.0 . 9.5 . 12 .
5052 H112 2.001–3.000 25.0 . 9.5 . 16 .
5052 H322 0.020–0.050 31.0 35.0 21.0 . 5 .
5052 H322 0.051–0.113 31.0 35.0 21.0 . 7 .
5052 H322 0.114–0.125 31.0 35.0 21.0 . 9 .
D
5052 F 0.250–3.000 . . . . . .
5059 O 0.078–0.249 48.0 . 23.0 . 24 .
5059 O 0.250–0.787 48.0 . 23.0 . 24 .
5059 O 0.788–1.575 48.0 . 23.0 . 20 .
5059 O 1.576–7.000 44.0 . 21.0 . 17 .
5059 H111 0.078–0.249 48.0 . 23.0 . 24 .
5059 H111 0.250–0.787 48.0 . 23.0 . 24 .
5059 H111 0.788–1.575 48.0 . 23.0 . 20 .
5059 H111 1.576–7.000 44.0 . 21.0 . 17 .
5083 O 0.051–1.500 40.0 51.0 18.0 29.0 16 .
5083 O 1.501–3.000 39.0 50.0 17.0 29.0 16 .
5083 O 3.001–4.000 38.0 . 16.0 . 16 .
5083 O 4.001–5.000 38.0 . 16.0 . 14 .
5083 O 5.001–7.000 37.0 . 15.0 . 14 .
5083 O 7.001–8.000 36.0 . 14.0 . 12 .
5083 H111 0.051–1.500 40.0 51.0 18.0 29.0 16 .
5083 H111 1.501–3.000 39.0 50.0 17.0 29.0 16 .
5083 H111 3.001–4.000 38.0 . 16.0 . 16 .
5083 H111 4.001–5.000 38.0 . 16.0 . 14 .
5083 H111 5.001–7.000 37.0 . 15.0 . 14 .
5083 H111 7.001–8.000 36.0 . 14.0 . 12 .
5083 H32 0.125–0.187 44.0 56.0 31.0 . 10 .
5083 H32 0.188–1.500 44.0 56.0 31.0 . 12 .
5083 H32 1.501–3.000 41.0 56.0 29.0 . 12 .
5083 H112 0.250–1.500 40.0 . 18.0 . 12 .
5083 H112 1.501–3.000 39.0 . 17.0 . 12 .
D
5083 F 0.250–8.000 . . . . . .
5086 O 0.020–0.050 35.0 44.0 14.0 . 15 .
5086 O 0.051–0.249 35.0 44.0 14.0 . 18 .
5086 O 0.250–2.000 35.0 44.0 14.0 . 16 .
C C
5086 H32 or H22 0.020–0.050 40.0 47.0 28.0 . 6 .
C C
5086 H32 or H22 0.051–0.249 40.0 47.0 28.0 . 8 .
C C
5086 H32 or H22 0.250–2.000 40.0 47.0 28.0 . 12 .
C C
5086 H34 or H24 0.009–0.019 44.0 51.0 34.0 . 4 .
C C
5086 H34 or H24 0.020–0.050 44.0 51.0 34.0 . 5 .
C C
5086 H34 or H24 0.051–0.249 44.0 51.0 34.0 . 6 .
C C
5086 H34 or H24 0.250–1.000 44.0 51.0 34.0 . 10 .
C C
5086 H36 or H26 0.006–0.019 47.0 54.0 38.0 . 3 .
C C
5086 H36 or H26 0.020–0.050 47.0 54.0 38.0 . 4 .
C C
5086 H36 or H26 0.051–0.162 47.0 54.0 38.0 . 6 .
C C
5086 H38 or H28 0.006–0.020 50.0 . 41.0 . 3 .
5086 H112 0.188–0.499 36.0 . 18.0 . 8 .
5086 H112 0.500–1.000 35.0 . 16.0 . 10 .
B209/B209M−21a
TABLE2 Continued
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi
Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
min max min max Factor, N
min, %
5086 H112 1.001–2.000 35.0 . 14.0 . 14 .
5086 H112 2.001–3.000 34.0 . 14.0 . 14 .
D
5086 F 0.250–3.000 . . . . . .
5154 O 0.020–0.031 30.0 41.0 11.0 . 12 .
5154 O 0.032–0.050 30.0 41.0 11.0 . 14 .
5154 O 0.051–0.113 30.0 41.0 11.0 . 16 .
5154 O 0.114–3.000 30.0 41.0 11.0 . 18 .
C C
5154 H32 or H22 0.020–0.050 36.0 43.0 26.0 . 5 .
C C
5154 H32 or H22 0.051–0.249 36.0 43.0 26.0 . 8 .
C C
5154 H32 or H22 0.250–2.000 36.0 43.0 26.0 . 12 .
C C
5154 H34 or H24 0.009–0.050 39.0 46.0 29.0 . 4 .
C C
5154 H34 or H24 0.051–0.161 39.0 46.0 29.0 . 6 .
C C
5154 H34 or H24 0.162–0.249 39.0 46.0 29.0 . 7 .
C C
5154 H34 or H24 0.250–1.000 39.0 46.0 29.0 . 10 .
C C
5154 H36 or H26 0.006–0.050 42.0 49.0 32.0 . 3 .
C C
5154 H36 or H26 0.051–0.113 42.0 49.0 32.0 . 4 .
C C
5154 H36 or H26 0.114–0.162 42.0 49.0 32.0 . 5 .
C C
5154 H38 or H28 0.006–0.050 45.0 . 35.0 . 3 .
C C
5154 H38 or H28 0.051–0.113 45.0 . 35.0 . 4 .
C C
5154 H38 or H28 0.114–0.128 45.0 . 35.0 . 5 .
5154 H112 0.250–0.499 32.0 . 18.0 . 8 .
5154 H112 0.500–2.000 30.0 . 11.0 . 11 .
5154 H112 2.001–3.000 30.0 . 11.0 . 15 .
D
5154 F 0.250–3.000 . . . . . .
5252 H24 0.030–0.090 30.0 38.0 . . 10 .
5252 H25 0.030–0.090 31.0 39.0 . . 9 .
5252 H28 0.030–0.090 38.0 . . . 3 .
5254 O 0.051–0.113 30.0 41.0 11.0 . 16 .
5254 O 0.114–3.000 30.0 41.0 11.0 . 18 .
C C
5254 H32 or H22 0.051–0.249 36.0 43.0 26.0 . 8 .
C C
5254 H32 or H22 0.250–2.000 36.0 43.0 26.0 . 12 .
C C
5254 H34 or H24 0.051–0.161 39.0 46.0 29.0 . 6 .
C C
5254 H34 or H24 0.162–0.249 39.0 46.0 29.0 . 7 .
C C
5254 H34 or H24 0.250–1.000 39.0 46.0 29.0 . 10 .
C C
5254 H36 or H26 0.051–0.113 42.0 49.0 32.0 . 4 .
C C
5254 H36 or H26 0.114–0.162 42.0 49.0 32.0 . 5 .
C C
5254 H38 or H28 0.051–0.113 45.0 . 35.0 . 4 .
C C
5254 H38 or H28 0.114–0.128 45.0 . 35.0 . 5 .
5254 H112 0.250–0.499 32.0 . 18.0 . 8 .
5254 H112 0.500–2.000 30.0 . 11.0 . 11 .
5254 H112 2.001–3.000 30.0 . 11.0 . 15 .
D
5254 F 0.250–3.000 . . . . . .
5454 O 0.020–0.031 31.0 41.0 12.0 . 12 .
5454 O 0.032–0.050 31.0 41.0 12.0 . 14 .
5454 O 0.051–0.113 31.0 41.0 12.0 . 16 .
5454 O 0.114–3.000 31.0 41.0 12.0 . 18 .
C C
5454 H32 or H22 0.020–0.050 36.0 44.0 26.0 . 5 .
C C
5454 H32 or H22 0.051–0.249 36.0 44.0 26.0 . 8 .
C C
5454 H32 or H22 0.250–2.000 36.0 44.0 26.0 . 12 .
C C
5454 H34 or H24 0.020–0.050 39.0 47.0 29.0 . 4 .
C C
5454 H34 or H24 0.051–0.161 39.0 47.0 29.0 . 6 .
C C
5454 H34 or H24 0.162–0.249 39.0 47.0 29.0 . 7 .
C C
5454 H34 or H24 0.250–1.000 39.0 47.0 29.0 . 10 .
5454 H112 0.250–0.499 32.0 . 18.0 . 8 .
5454 H112 0.500–2.000 31.0 . 12.0 . 11 .
5454 H112 2.001–3.000 31.0 . 12.0 . 15 .
D
5454 F 0.250–3.000 . . . . . .
5754 O 0.030–0.055 29.0 39.0 12.0 . 17 .
5754 O 0.056–0.087 29.0 39.0 12.0 . 18 .
5754 O 0.088–0.138 29.0 39.0 12.0 . 19 .
B209/B209M−21a
TABLE2 Continued
Elongation in
Tensile Strength, ksi Yield Strength (0.2 % offset), ksi
Bend
Specified 2 in. or 4×
Alloy Temper Diameter
Thickness, in. Diameter,
min max min max Factor, N
min, %
5456 O 0.051–1.500 42.0 53.0 19.0 30.0 16 .
5456 O 1.501–3.000 41.0 52.0 18.0 30.0 16 .
5456 O 3.001–5.000 40.0 . 17.0 . 14 .
5456 O 5.001–7.000 39.0 . 16.0 . 14 .
5456 O 7.001–8.000 38.0 . 15.0 . 12 .
5456 H32 0.188–0.499 46.0 59.0 33.0 . 12 .
5456 H32 0.500–1.500 44.0 56.0 31.0 . 12 .
5456 H32 1.501–3.000 41.0 54.0 29.0 . 12 .
5456 H112 0.250–1.500 42.0 . 19.0 . 12 .
5456 H112 1.501–3.000 41.0 . 18.0 . 12 .
D
5456 F 0.250–8.000 . . . . . .
5457 O 0.030–0.090 16.0 22.0 . . 20 .
F
5657 H241 0.030–0.090 18.0 26.0 . . 13 .
5657 H25 0.030–0.090 20.0 28.0 . . 8 .
5657 H26 0.030–0.090 22.0 30.0 . . 7 .
5657 H28 0.030–0.090 25.0 . . . 5 .
A
To determine conformance to this specification each value for tensile strength and yield strength shall be rounded to the nearest 0.1 ksi and each value for elongation
to the nearest 0.5 %, both in accordance with the Rounding Method of Practice E29.
B
The basis for establishment of mechanical property limits is shown in Annex A1.
C
Material in either of these tempers (H32 or H22), (H34 or H24), (H36 or H26), (H38 or H28), (H12 or H22), (H14 or H24), (H16 or H26), (H18 or H28), may be supplied
at the option of the supplier, unless one is specifically excluded by the contract or purchase order. When ordered as H2x tempers, the maximum tensile strength and
minimum yield strength do not apply. When H2x tempers are supplied instead of ordered H1x or H3x tempers, the supplied H2x temper material shall meet the respective
H1x or H3x temper tensile property limits.
D
Tests of F temper plate for tensile properties are not required.
E
The tension test specimen from plate 0.500 in. and thicker is machined from the core and does not include the cladding alloy.
F
This material is subject to some recrystallization and an attendant loss of brightness.
G
Mechanical property requirements for product outside the gauge range covered by Table 2 shall be agreed upon between purchaser and producer.
5.2.2 For nonheat-treated tempers, an inspection lot shall the same source of molten metal. If the producer has deter-
consist of an identifiable quantity of material of the same mill mined the chemical composition during pouring of the ingots,
form, alloy, temper, and thickness subjected to inspection at they shall not be required to sample and analyze the finished
one time. product.
NOTE 4—It is standard practice in the United States aluminum industry
6. General Quality
to determine conformance to the chemical composition limits prior to
6.1 Unless otherwise specified, the material shall be sup- further processing of ingots into wrought products. Due to the continuous
nature of the process, it is not practical to keep a specific ingot analysis
plied in the m
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