SAE 2219 Aluminium Alloys

Material group: Nonferrous Alloys / Aluminium Alloys

Country / Standard: United States / SAE

Indicative price:

Data updates

Latest Update: 2025-05

Total number of updates: 28

Update History

2024-09 2024-05 2023-05 2022-12 2022-02 2021-11 2021-02 2021-01 2020-07 2020-04 2020-03 2020-02 2019-04 2018-06 2018-03 2017-11 2017-10 2017-08 2017-04 2017-03 2017-02 2016-12 2015-11 2015-01 2014-04 2014-03 2013-12

This material has 1734 properties — only a subset is shown here.

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SAE 2219 Chemical Composition

CRITERIA

VALUE

UNIT

CAS NUMBER

CRITERIA

VALUE

5.8 – 6.8

UNIT

CAS NUMBER

7440-50-8

CRITERIA

VALUE

≤ 0.30

UNIT

CAS NUMBER

7439-89-6

CRITERIA

VALUE

≤ 0.02

UNIT

CAS NUMBER

7439-95-4

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7439-96-5

CRITERIA

Other each

VALUE

val1

UNIT

CAS NUMBER

CRITERIA

Other total

VALUE

val1

UNIT

CAS NUMBER

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-21-3

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-32-6

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-62-2

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-66-6

CRITERIA

VALUE

val1

UNIT

CAS NUMBER

7440-67-7

SAE AMS 4163G: 2022 / Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T3511) Solution Heat Treated, Stress-Relieved by Stretching, and Straightened

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SAE 2219 Physical Properties

Temperature

≤ 0°C 0 - 30°C 30 - 100°C 100 - 300°C ≥ 300°C

PROPERTY / VALUE

Compression Modulus

72 — 74 GPa

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Modulus of Elasticity

69 — 79 GPa

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Thermal Conductivity

val1 W/(m∙°C)

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Electrical Resistivity

0.057 — 0.062 Ω∙mm²/m

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Density

val1 kg/dm³

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Heat Capacity

val1 J/(kg∙°C)

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Electrical Conductivity

val1 S/m

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Poisson Coefficient

val1

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Shear Modulus

val1 GPa

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Coefficient of Thermal Expansion (CTE)

val1 10^-6/°C

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This material has 1734 properties — only a subset is shown here.

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SAE 2219 Heat Treatments

Rings shall be solution heat treated and mechanically stress-relieved, to the T351 or T352 condition as applicable.
Type 1 - Solution heat treated and stress relieved by stretching to produce a permanent set of 1-1/2 to 5%.
Type 2 - Solution heat treated and stress relieved by compression to produce a permanent set of 1-1/2 to 5%. During compression, primary forces shall be applied in the axial direction.
Solution heat treating at 535°C for all forms.
Limits for quenching in polymer solutions for sheets and extrusions: for thickness 1.85 mm polymer concentration is 22% max (±2).
Aging treatment is mandatory. For alclad sheets: Starting temper is T42, final temper is T62 (sometimes used to designate final tempers), aging at 191°C for 17-19h. For forgings, Starting temper is T42 or T4, final temper is T62 or T6 (sometimes used to designate final tempers), aging 191°C for 25-27h; Starting temper is T352, final temper is T852 (sometimes used to designate final tempers), aging 177°C for 17-19h. For sheets, Starting temper is T31, final temper is T81 (sometimes used to designate final tempers), aging 177°C for 17-19h; Starting temper is T37, final temper is T87 (sometimes used to designate final tempers), aging 163°C for 23-25h. For plates, Starting temper is T351, final temper is T851 (sometimes used to designate final tempers), aging 177°C for 17-19h; Starting temper is T37, final temper is T87 (sometimes used to designate final tempers), aging 163°C for 17-19h. For rivets: Starting temper is T31, final temper is T81 (sometimes used to designate final tempers), aging at 177°C for 17-19h. For extruded bars and shapes: Starting temper is T31 or T351X, final temper is T81 or T851X (sometimes used to designate final tempers), aging at 191°C for 17-19h. For all others forms: Starting temper is T42, final temper is T62 (sometimes used to designate final tempers), aging at 191°C for 35-37h. When temper before furnace aging is T4 or T42, the furnace aging treatment may be started immediately after quenching or at any time thereafter.
Full anneal: At 399-427°C, soaking time is minimum 1h (soak times listed are for up to 13 mm maximum thickness. Add 0.5 hour for each additional 13 mm of product or nested stack thickness or fraction thereof over 13 mm), cooling in furnace (furnace cool at 28°C degrees per hour maximum, to 260°C, air cool to room temperature or furnace cool at 28°C degrees per hour maximum, to 232°C, hold at 232°C for 6 hours, furnace or air cool to room temperature). Stress relief: At 333-349°C, soaking time is minimum 0.5h (soak times listed are for up to 13 mm maximum thickness. Add 0.5 hour for each additional 13 mm of product or nested stack thickness or fraction thereof over 13 mm), cooling in air.
Solution heat treating soaking times and maximum quench delay times is on specifications.

SAE 2219 Mechanical Properties

Temperature

0 - 30°C

PROPERTY / VALUE

Tensile Strength

≥ 152 MPa

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Brinell Hardness (HB)

77 — 115

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Compression Yield Strength

val1 MPa

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Elongation, A

≥ 2 %

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Yield Strength, Rp0.2

val1 MPa

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SAE 2219 International Equivalent Materials

Showing 15 of 111 results.

MATERIAL

STANDARD

COUNTRY / PRODUCER

EQUIVALENCE CATEGORY

MATERIAL

A92219

STANDARD

UNS

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Official

MATERIAL

2219

STANDARD

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

AL-P2219-O, -H111, -T62

STANDARD

AFNOR NF

COUNTRY / PRODUCER

France

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

EN AW-2219

STANDARD

COUNTRY / PRODUCER

European Union

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

EN AW-Al Cu6Mn

STANDARD

COUNTRY / PRODUCER

European Union

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

2219

STANDARD

COUNTRY / PRODUCER

China

EQUIVALENCE CATEGORY

Official

MATERIAL

AL-P2219-T31, -T81

STANDARD

AFNOR NF

COUNTRY / PRODUCER

France

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

SB-211 2219

STANDARD

ASME

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

SB-241 2219

STANDARD

ASME

COUNTRY / PRODUCER

United States

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

1201

STANDARD

GOST

COUNTRY / PRODUCER

Russia

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

AlCu6Mn

STANDARD

ISO

COUNTRY / PRODUCER

International

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

A 2219 FD

STANDARD

JIS

COUNTRY / PRODUCER

Japan

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

A 2219 FH

STANDARD

JIS

COUNTRY / PRODUCER

Japan

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

A 2219P

STANDARD

JIS

COUNTRY / PRODUCER

Japan

EQUIVALENCE CATEGORY

Composition 100%

MATERIAL

L-3191

STANDARD

UNE

COUNTRY / PRODUCER

Spain

EQUIVALENCE CATEGORY

Composition 100%

Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.

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111Cross References

189Composition
874Mechanical Properties
78Physical Properties
4Heat Treatment
-Metallography
-Machinability

281Stress-Strain
1Formability
96Fatigue
22Fracture
13Creep

2Joints
-Coatings
-Dimensions
-Tribology

-Corrosion
18Ageing
-Weatherability
-Irradiation

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