Aluminum Round Bars Customized with Your Demand – Size OD35mm x 3m Length is now in stock, competitive price, good service, fast delivery, flexible payment.

List of Aluminium Alloys

1000 series (essentially pure)

1000 series are essentially pure aluminium with a minimum 99% aluminium content by weight and can be work hardened. 1000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al contents	Alloying elements	Uses and refs
1050	99.5	–	Drawn tube, chemical equipment
1060	99.6	–	Universal
1070	99.7	–	Thick-wall drawn tube
1100	99.0	Cu 0.1	Universal, holloware
1145	99.45	–	Sheet, plate, foil
1199	99.99	–	Foil
1200	99.0 max	(Si + Fe) 1.0 max; Cu 0.05 max; Mn 0.05 max; Zn 0.10 max; Ti 0.05 max; others 0.05 (each) .015 (total)
1230 (VAD23)#		Si 0.3; Fe 0.3; Cu 4.8–5.8; Mn 0.4–0.8; Mg 0.05; Zn 0.1; Ti 0.15; Li 0.9–1.4; Cd 0.1–0.25	Tu-144 aircraft
1350	99.5	–	Electrical conductors
1370	99.7	–	Electrical conductors
1420#	92.9	Mg 5.0; Li 2.0; Zr 0.1	Aerospace
1421#	92.9	Mg 5.0; Li 2.0; Mn 0.2; Sc 0.2; Zr 0.1	Aerospace
1424#		Si 0.08; Fe 0.1; Mn 0.1–0.25; Mg 4.7–5.2; Zn 0.4–0.7; Li 1.5–1.8; Zr 0.07–0.1; Be 0.02–0.2; Sc 0.05–0.08; Na 0.0015
1430#		Si 0.1; Fe 0.15; Cu 1.4–1.8; Mn 0.3–0.5; Mg 2.3–3.0; Zn 0.5–0.7; Ti 0.01–0.1; Li 1.5–1.9; Zr 0.08–0.14; Be 0.02–0.1; Sc 0.01–0.1; Na 0.003; Ce 0.2–0.4; Y 0.05–0.1
1440#		Si 0.02–0.1; Fe 0.03–0.15; Cu 1.2–1.9; Mn 0.05; Mg 0.6–1.1; Cr 0.05; Ti 0.02–0.1; Li 2.1–2.6; Zr 0.10–0.2; Be 0.05–0.2; Na 0.003
1441#		Si 0.08; Fe 0.12; Cu 1.5–1.8; Mn 0.001–0.010; Mg 0.7–1.1; Ti 0.01–0.07; Ni 0.02–0.10; Li 1.8–2.1; Zr 0.04–0.16; Be 0.02–0.20	Be-103 and Be-200 hydroplanes
1441K#		Si 0.08; Fe 0.12; Cu 1.3–1.5; Mn 0.001–0.010; Mg 0.7–1.1; Ti 0.01–0.07; Ni 0.01–0.15; Li 1.8–2.1; Zr 0.04–0.16; Be 0.002–0.01
1445#		Si 0.08; Fe 0.12; Cu 1.3–1.5; Mn 0.001–0.010; Mg 0.7–1.1; Ti 0.01–0.1; Ni 0.01–0.15; Li 1.6–1.9; Zr 0.04–0.16; Be 0.002–0.01; Sc 0.005–0.001; Ag 0.05–0.15; Ca 0.005–0.04; Na 0.0015
1450#		Si 0.1; Fe 0.15; Cu 2.6–3.3; Mn 0.1; Mg 0.1; Cr 0.05; Zn 0.25; Ti 0.01–0.06; Li 1.8–2.3; Zr 0.08–0.14; Be 0.008–0.1; Na 0.002; Ce 0.005–0.05	An-124 and An-225 aircraft
1460#		Si 0.1; Fe 0.03–0.15; Cu 2.6–3.3; Mg 0.05; Ti 0.01–0.05; Li 2.0–2.4; Zr 0.08–0.13; Na 0.002; Sc 0.05–0.14; B 0.0002–0.0003	Tu-156 aircraft
V-1461#		Si 0.8; Fe 0.01–0.1; Cu 2.5–2.95; Mn 0.2–0.6; Mg 0.05–0.6; Cr 0.01–0.05; Zn 0.2–0.8; Ti 0.05; Ni 0.05–0.15; Li 1.5–1.95; Zr 0.05–0.12; Be 0.0001–0.02; Sc 0.05–0.10; Ca 0.001–0.05; Na 0.0015
V-1464#		Si 0.03–0.08; Fe 0.03–0.10; Cu 3.25–3.45; Mn 0.20–0.30; Mg 0.35–0.45; Ti 0.01–0.03; Li 1.55–1.70; Zr 0.08–0.10; Sc 0.08–0.10; Be 0.0003–0.02; Na 0.0005
V-1469#		Si 0.1; Fe 0.12; Cu 3.2–4.5; Mn 0.003–0.5; Mg 0.1–0.5; Li 1.0–1.5; Zr 0.04–0.20; Sc 0.04–0.15; Ag 0.15–0.6

# Not an International Alloy Designation System name

2000 series (copper)

2000 series are alloyed with copper, can be precipitation hardened to strengths comparable to steel. Formerly referred to as duralumin, they were once the most common aerospace alloys, but were susceptible to stress corrosion cracking and are increasingly replaced by 7000 series in new designs. 2000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al contents	Alloying elements	Uses and refs
2004	93.6	Cu 6.0; Zr 0.4	Aerospace
2011	93.7	Cu 5.5; Bi 0.4; Pb 0.4	Universal
2014	93.5	Cu 4.4; Si 0.8; Mn 0.8; Mg 0.5	Universal
2017	94.2	Cu 4.0; Si 0.5; Mn 0.7; Mg 0.6	Aerospace
2020	93.4	Cu 4.5; Li 1.3; Mn 0.55; Cd 0.25	Aerospace
2024	93.5	Cu 4.4; Mn 0.6; Mg 1.5	Universal, aerospace
2029	94.6	Cu 3.6; Mn 0.3; Mg 1.0; Ag 0.4; Zr 0.1	Alclad sheet, aerospace
2036	96.7	Cu 2.6; Mn 0.25; Mg 0.45	Sheet
2048	94.8	Cu 3.3; Mn 0.4; Mg 1.5	Sheet, plate
2055	93.5	Cu 3.7; Zn 0.5; Li 1.1; Ag 0.4;Mn 0.2; Mg 0.3; Zr 0.1	Aerospace extrusions
2080	94.0	Mg 3.7; Zn 1.85; Cr 0.2; Li 0.2	Aerospace
2090	95.0	Cu 2.7; Li 2.2; Zr 0.12	Aerospace
2091	94.3	Cu 2.1; Li 2.0; Mg 1.5; Zr 0.1	Aerospace, cryogenics
2094		Si 0.12; Fe 0.15; Cu 4.4–5.2; Mn 0.25; Mg 0.25–0.8; Zn 0.25; Ti 0.10; Ag 0.25–0.6; Li 0.7–1.4; Zr 0.04–0.18
2095	93.6	Cu 4.2; Li 1.3; Mg 0.4; Ag 0.4; Zr 0.1	Aerospace
2097		Si 0.12; Fe 0.15; Cu 2.5–3.1; Mn 0.10–0.6; Mg 0.35; Zn 0.35; Ti 0.15; Li 1.2–1.8; Zr 0.08–0.15
2098		Si 0.12; Fe 0.15; Cu 2.3–3.8; Mn 0.35; Mg 0.25–0.8; Zn 0.35; Ti 0.10; Ag 0.25–0.6; Li 2.4–2.8; Zr 0.04–0.18
2099	94.3	Cu 2.53; Mn 0.3; Mg 0.25; Li 1.75; Zn 0.75; Zr 0.09	Aerospace
2124	93.5	Cu 4.4; Mn 0.6; Mg 1.5	Plate
2195	93.5	Cu 4.0; Mn 0.5; Mg 0.45; Li 1.0; Ag 0.4; Zr 0.12	aerospace, Space Shuttle Super Lightweight external tank, and the SpaceX Falcon 9 and Falcon 1e second stage launch vehicles.
2196		Si 0.12; Fe 0.15; Cu 2.5–3.3; Mn 0.35; Mg 0.25–0.8; Zn 0.35; Ti 0.10; Ag 0.25–0.6; Li 1.4–2.1; Zr 0.08–0.16	Extrusion
2197		Si 0.10; Fe 0.10; Cu 2.5–3.1; Mn 0.10–0.50; Mg 0.25; Zn 0.05; Ti 0.12; Li 1.3–1.7; Zr 0.08–0.15
2198			Sheet
2218	92.2	Cu 4.0; Mg 1.5; Fe 1.0; Si 0.9; Zn 0.25; Mn 0.2	Forgings, aircraft engine cylinders
2219	93.0	Cu 6.3; Mn 0.3;Ti 0.06; V 0.1; Zr 0.18	Universal, Space Shuttle Standard Weight external tank
2297		Si 0.10; Fe 0.10; Cu 2.5–3.1; Mn 0.10–0.50; Mg 0.25; Zn 0.05; Ti 0.12; Li 1.1–1.7; Zr 0.08–0.15
2397		Si 0.10; Fe 0.10; Cu 2.5–3.1; Mn 0.10–0.50; Mg 0.25; Zn 0.05–0.15; Ti 0.12; Li 1.1–1.7; Zr 0.08–0.15
2224&2324	93.8	Cu 4.1; Mn 0.6; Mg 1.5	Plate
2319	93.0	Cu 6.3; Mn 0.3; Ti 0.15; V 0.1; Zr 0.18	Bar and wire
2519	93.0	Cu 5.8; Mg 0.2; Ti 0.15; V 0.1; Zr 0.2	Aerospace armour plate
2524	93.8	Cu 4.2; Mn 0.6; Mg 1.4	Plate, sheet
2618	93.7	Cu 2.3; Si 0.18; Mg 1.6; Ti 0.07; Fe 1.1; Ni 1.0	Forgings

3000 series (manganese)

3000 series are alloyed with manganese, and can be work hardened. 3000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al contents	Alloying elements	Uses and refs
3003	98.6	Mn 1.5; Cu 0.12	Universal, sheet, rigid foil containers, signs, decorative
3004	97.8	Mn 1.2; Mg 1	Universal, beverage cans
3005	98.5	Mn 1.0; Mg 0.5	Work-hardened
3102	99.8	Mn 0.2	Work-hardened
3103&3303	98.8	Mn 1.2	Work-hardened
3105	97.8	Mn 0.55; Mg 0.5	Sheet
3203	98.8	Mn 1.2	Sheet, high strength foil

4000 series (silicon)

4000 series are alloyed with silicon. Variations of aluminium–silicon alloys intended for casting (and therefore not included in 4000 series) are also known as silumin. 4000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al contents	Alloying elements	Uses and refs
4006	98.3	Si 1.0; Fe 0.65	Work-hardened or aged
4007	96.3	Si 1.4; Mn 1.2; Fe 0.7; Ni 0.3; Cr 0.1	Work-hardened
4015	96.8	Si 2.0; Mn 1.0; Mg 0.2	Work-hardened
4032	85	Si 12.2; Cu 0.9; Mg 1; Ni 0.9;	Forgings
4043	94.8	Si 5.2	Rod
4047	85.5	Si 12.0; Fe 0.8; Cu 0.3; Zn 0.2; Mn 0.15; Mg 0.1	Sheet, cladding, fillers
4543	93.7	Si 6.0; Mg 0.3	architectural extrusions

5000 series (magnesium)

5000 series are alloyed with magnesium, and offer superb corrosion resistance, making them suitable for marine applications. Also, 5083 alloy has the highest strength of not heat-treated alloys. Most 5000 series alloys include manganese as well. 5000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al contents	Alloying elements	Uses and refs
5005 & 5657	99.2	Mg 0.8	Sheet, plate, rod
5010	99.3	Mg 0.5; Mn 0.2;
5019	94.7	Mg 5.0; Mn 0.25;
5024	94.5	Mg 4.6; Mn 0.6; Zr 0.1; Sc 0.2	Extrusions, aerospace
5026	93.9	Mg 4.5; Mn 1; Si 0.9; Fe 0.4; Cu 0.3
5050	98.6	Mg 1.4	Universal
5052 & 5652	97.2	Mg 2.5; Cr 0.25	Universal, aerospace, marine
5056	94.8	Mg 5.0; Mn 0.12; Cr 0.12	Foil, rod, rivets
5059	93.5	Mg 5.0; Mn 0.8; Zn 0.6; Zr 0.12	rocket cryogenic tanks
5083	94.8	Mg 4.4; Mn 0.7; Cr 0.15	Universal, welding, marine
5086	95.4	Mg 4.0; Mn 0.4; Cr 0.15	Universal, welding, marine
5154 & 5254	96.2	Mg 3.5; Cr 0.25;	Universal, rivets
5182	95.2	Mg 4.5; Mn 0.35;	Sheet
5252	97.5	Mg 2.5;	Sheet
5356	94.6	Mg 5.0; Mn 0.12; Cr 0.12; Ti 0.13	Rod, MIG wire
5454	96.4	Mg 2.7; Mn 0.8; Cr 0.12	Universal
5456	94	Mg 5.1; Mn 0.8; Cr 0.12	Universal
5457	98.7	Mg 1.0; Mn 0.2; Cu 0.1	Sheet, automobile trim
5557	99.1	Mg 0.6; Mn 0.2; Cu 0.1	Sheet, automobile trim
5754	95.8	Mg 3.1; Mn 0.5; Cr 0.3	Sheet, Rod

6000 series (magnesium and silicon)

6000 series are alloyed with magnesium and silicon. They are easy to machine, are weldable, and can be precipitation hardened, but not to the high strengths that 2000 and 7000 can reach. 6061 alloy is one of the most commonly used general-purpose aluminium alloys. 6000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al contents	Alloying elements	Uses and refs
6005	98.7	Si 0.8; Mg 0.5	Extrusions, angles
6009	97.7	Si 0.8; Mg 0.6; Mn 0.5; Cu 0.35	Sheet
6010	97.3	Si 1.0; Mg 0.7; Mn 0.5; Cu 0.35	Sheet
6013	97.05	Si 0.8; Mg 1.0; Mn 0.35; Cu 0.8	Plate, aerospace, smartphone cases
6022	97.9	Si 1.1; Mg 0.6; Mn 0.05; Cu 0.05; Fe 0.3	Sheet, automotive
6060	98.9	Si 0.4; Mg 0.5; Fe 0.2	Heat-treatable
6061	97.9	Si 0.6; Mg 1.0; Cu 0.25; Cr 0.2	Universal, structural, aerospace
6063 & 646g	98.9	Si 0.4; Mg 0.7	Universal, marine, decorative
6063A	98.7	Si 0.4; Mg 0.7; Fe 0.2	Heat-treatable
6065	97.1	Si 0.6; Mg 1.0; Cu 0.25; Bi 1.0	Heat-treatable
6066	95.7	Si 1.4; Mg 1.1; Mn 0.8; Cu 1.0	Universal
6070	96.8	Si 1.4; Mg 0.8; Mn 0.7; Cu 0.28	Extrusions
6081	98.1	Si 0.9; Mg 0.8; Mn 0.2	Heat-treatable
6082	97.5	Si 1.0; Mg 0.85; Mn 0.65	Heat-treatable
6101	98.9	Si 0.5; Mg 0.6	Extrusions
6105	98.6	Si 0.8; Mg 0.65	Heat-treatable
6113	96.8	Si 0.8; Mg 1.0; Mn 0.35; Cu 0.8; O 0.2	Aerospace
6151	98.2	Si 0.9; Mg 0.6; Cr 0.25	Forgings
6162	98.6	Si 0.55; Mg 0.9	Heat-treatable
6201	98.5	Si 0.7; Mg 0.8	Rod
6205	98.4	Si 0.8; Mg 0.5;Mn 0.1; Cr 0.1; Zr 0.1	Extrusions
6262	96.8	Si 0.6; Mg 1.0; Cu 0.25; Cr 0.1; Bi 0.6; Pb 0.6	Universal
6351	97.8	Si 1.0; Mg 0.6;Mn 0.6	Extrusions
6463	98.9	Si 0.4; Mg 0.7	Extrusions
6951	97.2	Si 0.5; Fe 0.8; Cu 0.3; Mg 0.7; Mn 0.1; Zn 0.2	Heat-treatable

7000 series (zinc)

7000 series are alloyed with zinc, and can be precipitation hardened to the highest strengths of any aluminium alloy (ultimate tensile strength up to 700 MPa for the 7068 alloy). Most 7000 series alloys include magnesium and copper as well. 7000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al contents	Alloying elements	Uses and refs
7005	93.3	Zn 4.5; Mg 1.4; Mn 0.45; Cr 0.13; Zr 0.14; Ti 0.04	Extrusions
7010	93.3	Zn 6.2; Mg 2.35; Cu 1.7; Zr 0.1;	Aerospace
7022	91.1	Zn 4.7; Mg 3.1; Mn 0.2; Cu 0.7; Cr 0.2;	plate, molds
7034	85.7	Zn 11.0; Mg 2.3; Cu 1.0	Ultimate tensile strength 750 Mpa
7039	92.3	Zn 4.0; Mg 3.3; Mn 0.2; Cr 0.2	Aerospace armour plate
7049	88.1	Zn 7.7; Mg 2.45; Cu 1.6; Cr 0.15	Universal, aerospace
7050	89.0	Zn 6.2; Mg 2.3; Cu 2.3; Zr 0.1	Universal, aerospace
7055	87.2	Zn 8.0; Mg 2.3; Cu 2.3; Zr 0.1	Plate, extrusions, aerospace
7065	88.5	Zn 7.7; Mg 1.6; Cu 2.1; Zr 0.1	Plate, aerospace
7068	87.6	Zn 7.8; Mg 2.5; Cu 2.0; Zr 0.12	Aerospace, Ultimate tensile strength 710 MPa
7072	99.0	Zn 1.0	Sheet, foil
7075 & 7175	90.0	Zn 5.6; Mg 2.5; Cu 1.6; Cr 0.23	Universal, aerospace, forgings
7079	91.4	Zn 4.3; Mg 3.3; Cu 0.6; Mn 0.2; Cr 0.15	-
7085	89.4	Zn 7.5; Mg 1.5; Cu 1.6	Thick plate, aerospace
7090		Al-Zn-Mg-Cu with Co 1.5%	high strength, ductility and resistance to stress corrosion cracking
7091		Al-Zn-Mg-Cu with Co 0.4%	high strength, ductility and resistance to stress corrosion cracking
7093	86.7	Zn 9.0; Mg 2.5; Cu 1.5; O 0.2; Zr 0.1	Aerospace
7116	93.7	Zn 4.5; Mg 1; Cu 0.8	Heat-treatable
7129	93.2	Zn 4.5; Mg 1.6; Cu 0.7	-
7150	89.05	Zn 6.4; Mg 2.35; Cu 2.2; O 0.2; Zr 0.1	Aerospace
7178	88.1	Zn 6.8; Mg 2.7; Cu 2.0; Cr 0.26	Universal, aerospace
7255	87.5	Zn 8.0; Mg 2.1; Cu 2.3; Zr 0.1	Plate, aerospace
7475	90.3	Zn 5.7; Mg 2.3; Si 1.5; Cr 0.22	Universal, aerospace

8000 series (other elements)

8000 series are alloyed with other elements which are not covered by other series. Aluminium–lithium alloys are an example. 8000 series aluminium alloy nominal composition (% weight) and applications

Alloy	Al content	Alloying elements	Uses and refs
8006	98.0	Fe 1.5; Mn 0.5;	Universal, weldable
8009	88.3	Fe 8.6; Si 1.8; V 1.3	High-temperature aerospace
8011	98.7	Fe 0.7; Si 0.6	Work-hardened
8014	98.2	Fe 1.4; Mn 0.4;	universal
8019	87.5	Fe 8.3; Ce 4.0; O 0.2	Aerospace
8025		Si 0.05; Fe 0.06–0.25; Cu 0.20; Mg 0.05; Cr 0.18; Zn 0.50; Ti 0.005–0.02; Li 3.4–4.2; Zr 0.08–0.25
8030	99.3	Fe 0.5; Cu 0.2	wire
8090		Si 0.20; Fe 0.30; Cu 1.0–1.6; Mn 0.10; Mg 0.6–1.3; Cr 0.10; Zn 0.25; Ti 0.10; Li 2.2–2.7; Zr 0.04–0.16
8091		Si 0.30; Fe 0.50; Cu 1.0–1.6; Mn 0.10; Mg 0.50–1.2; Cr 0.10; Zn 0.25; Ti 0.10; Li 2.4–2.8; Zr 0.08–0.16
8093		Si 0.10; Fe 0.10; Cu 1.6–2.2; Mn 0.10; Mg 0.9–1.6; Cr 0.10; Zn 0.25; Ti 0.10; Li 1.9–2.6; Zr 0.04–0.14
8176	99.3	Fe 0.6; Si 0.1	electrical wire

Aluminium Alloys Composition Limits

Alloy	Si	Fe	Cu	Mn	Mg	Cr	Zn	V	Ti	Bi	Ga	Pb	Zr	Limits††		Al
														Each	Total
1050	0.25	0.40	0.05	0.05	0.05			0.05						0.03		99.5 min
1060	0.25	0.35	0.05	0.028	0.03	0.03	0.05	0.05	0.028	0.03	0.03	0.03	0.03	0.028		99.6 min
1100	0.95 Si+Fe		0.05–0.20	0.05			0.10							0.05	0.15	99.0 min
1199	0.006	0.006	0.006	0.002	0.006		0.006	0.005	0.002		0.005			0.002		99.99 min
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
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
2219	0.2	0.30	5.8–6.8	0.20–0.40	0.02		0.10	0.05–0.15	0.02–0.10				0.10–0.25	0.05	0.15	remainder
3003	0.6	0.7	0.05–0.20	1.0–1.5			0.10							0.05	0.15	remainder
3004	0.30	0.7	0.25	1.0–1.5	0.8–1.3		0.25							0.05	0.15	remainder
3102	0.40	0.7	0.10	0.05–0.40			0.30		0.10					0.05	0.15	remainder
4043	4.5–6.0	0.80	0.30	0.05	0.05		0.10		0.20					0.05	0.15	remainder
5005	0.3	0.7	0.2	0.2	0.5–1.1	0.1	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
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	3.10–3.90	0.15–0.35	0.20		0.20					0.05	0.15	remainder
5356	0.25	0.40	0.10	0.10	4.50–5.50	0.05–0.20	0.10		0.06–0.20					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
5754	0.40	0.40	0.10	0.50	2.6–3.6	0.30	0.20		0.15					0.05	0.15	remainder
6005	0.6–0.9	0.35	0.10	0.10	0.40–0.6	0.10	0.10		0.10					0.05	0.15	remainder
6005A†	0.50–0.9	0.35	0.30	0.50	0.40–0.7	0.30	0.20		0.10					0.05	0.15	remainder
6060	0.30–0.6	0.10–0.30	0.10	0.10	0.35–0.6	0.05	0.15		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
6063	0.20–0.6	0.35	0.10	0.10	0.45–0.9	0.10	0.10		0.10					0.05	0.15	remainder
6066	0.9–1.8	0.50	0.7–1.2	0.6–1.1	0.8–1.4	0.40	0.25		0.20					0.05	0.15	remainder
6070	1.0–1.7	0.50	0.15–0.40	0.40–1.0	0.50–1.2	0.10	0.25		0.15					0.05	0.15	remainder
6082	0.7–1.3	0.50	0.10	0.40–1.0	0.60–1.2	0.25	0.20		0.10					0.05	0.15	remainder
6105	0.6–1.0	0.35	0.10	0.10	0.45–0.8	0.10	0.10		0.10					0.05	0.15	remainder
6162	0.40–0.8	0.50	0.20	0.10	0.7–1.1	0.10	0.25		0.10					0.05	0.15	remainder
6262	0.40–0.8	0.7	0.15–0.40	0.15	0.8–1.2	0.04–0.14	0.25		0.15	0.40–0.7		0.40–0.7		0.05	0.15	remainder
6351	0.7–1.3	0.50	0.10	0.40–0.8	0.40–0.8		0.20		0.20					0.05	0.15	remainder
6463	0.20–0.6	0.15	0.20	0.05	0.45–0.9		0.05							0.05	0.15	remainder
7005	0.35	0.40	0.10	0.20–0.70	1.0–1.8	0.06–0.20	4.0–5.0		0.01–0.06				0.08–0.20	0.05	0.15	remainder
7022	0.50	0.50	0.50–1.00	0.10–0.40	2.60–3.70	0.10–0.30	4.30–5.20		0.20					0.05	0.15	remainder
7068	0.12	0.15	1.60–2.40	0.10	2.20–3.00	0.05	7.30–8.30		0.01				0.05–0.15	0.05	0.15	remainder
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
7079	0.3	0.40	0.40–0.80	0.10–0.30	2.9–3.7	0.10–0.25	3.8–4.8		0.10					0.05	0.15	remainder
7116	0.15	0.30	0.50–1.1	0.05	0.8–1.4		4.2–5.2	0.05	0.05		0.03			0.05	0.15	remainder
7129	0.15	0.30	0.50–0.9	0.10	1.3–2.0	0.10	4.2–5.2	0.05	0.05		0.03			0.05	0.15	remainder
7178	0.40	0.50	1.6–2.4	0.30	2.4–3.1	0.18–0.28	6.3–7.3		0.20					0.05	0.15	remainder
8176[46]	0.03–0.15	0.40–1.0					0.10				0.03			0.05	0.15	remainder
Alloy	Si	Fe	Cu	Mn	Mg	Cr	Zn	V	Ti	Bi	Ga	Pb	Zr	Limits††		Al
														Each	Total

†Manganese plus chromium must be between 0.12 and 0.50%. ††This limit applies to all elements for which no other limit is specified on a given row, because no column exists or because the column is blank.

Minimum tensile requirements for cast aluminium alloys

Alloy type		Temper	Tensile strength (min) in ksi (MPa)	Yield strength (min) in ksi (MPa)	Elongation in 2 in %
ANSI	UNS
201.0	A02010	T7	60.0 (414)	50.0 (345)	3.0
204.0	A02040	T4	45.0 (310)	28.0 (193)	6.0
242.0	A02420	O	23.0 (159)	N/A	N/A
		T61	32.0 (221)	20.0 (138)	N/A
A242.0	A12420	T75	29.0 (200)	N/A	1.0
295.0	A02950	T4	29.0 (200)	13.0 (90)	6.0
		T6	32.0 (221)	20.0 (138)	3.0
		T62	36.0 (248)	28.0 (193)	N/A
		T7	29.0 (200)	16.0 (110)	3.0
319.0	A03190	F	23.0 (159)	13.0 (90)	1.5
		T5	25.0 (172)	N/A	N/A
		T6	31.0 (214)	20.0 (138)	1.5
328.0	A03280	F	25.0 (172)	14.0 (97)	1.0
		T6	34.0 (234)	21.0 (145)	1.0
355.0	A03550	T6	32.0 (221)	20.0 (138)	2.0
		T51	25.0 (172)	18.0 (124)	N/A
		T71	30.0 (207)	22.0 (152)	N/A
C355.0	A33550	T6	36.0 (248)	25.0 (172)	2.5
356.0	A03560	F	19.0 (131)	9.5 (66)	2.0
		T6	30.0 (207)	20.0 (138)	3.0
		T7	31.0 (214)	N/A	N/A
		T51	23.0 (159)	16.0 (110)	N/A
		T71	25.0 (172)	18.0 (124)	3.0
A356.0	A13560	T6	34.0 (234)	24.0 (165)	3.5
		T61	35.0 (241)	26.0 (179)	1.0
443.0	A04430	F	17.0 (117)	7.0 (48)	3.0
B443.0	A24430	F	17.0 (117)	6.0 (41)	3.0
512.0	A05120	F	17.0 (117)	10.0 (69)	N/A
514.0	A05140	F	22.0 (152)	9.0 (62)	6.0
520.0	A05200	T4	42.0 (290)	22.0 (152)	12.0
535.0	A05350	F	35.0 (241)	18.0 (124)	9.0
705.0	A07050	T5	30.0 (207)	17.0 (117)†	5.0
707.0	A07070	T7	37.0 (255)	30.0 (207)†	1.0
710.0	A07100	T5	32.0 (221)	20.0 (138)	2.0
712.0	A07120	T5	34.0 (234)	25.0 (172)†	4.0
713.0	A07130	T5	32.0 (221)	22.0 (152)	3.0
771.0	A07710	T5	42.0 (290)	38.0 (262)	1.5
		T51	32.0 (221)	27.0 (186)	3.0
		T52	36.0 (248)	30.0 (207)	1.5
		T6	42.0 (290)	35.0 (241)	5.0
		T71	48.0 (331)	45.0 (310)	5.0
850.0	A08500	T5	16.0 (110)	N/A	5.0
851.0	A08510	T5	17.0 (117)	N/A	3.0
852.0	A08520	T5	24.0 (165)	18.0 (124)	N/A

†Only when requested by the customer Source: Wiki

See more...