Aluminium 2000
We are leading manufacturer and stockist of Aluminium 2000 in China.Aluminium 2000 / Aluminium Alloy 2011 Aluminium 2000 / Aluminium Alloy 2011 Technical Data SheetAluminium 2000 / Aluminium Alloy 2011 Chemical Composition LimitsWeight%AlSiFeCuZnBiPbOthers2011Bal0.40 max0.70 max5.0-6.00.30 max0.20-0.600.20-0.600.05 (each)
0.15 (total)Aluminium 2011 is a heat treatable high strength alloy with high fatigue strength and excellent free machining characteristics. Due to the high copper content of Alloy 2011 makes it the best choice for aluminium machining. Alloy 2011 is used for screws,Website:, bolts, fittings, nuts, automatic lathe and screw machine products.Aluminium 2000 / Aluminium Alloy 2011 Mechanical PropertiesMaterialTempsThickness (min)Tensile Strength (N/mm²) minYield Strength (N/mm²) minElongation on 50mm (%)2011 BarTD< BarTD BarTD BarTF< BarTF>652951958Aluminium 2000 / Aluminium Alloy 2011 Specifications
Similar Specifications
BS FC1
Alcoa-800
AWCO-308
BA 308
Durcilium-L
Hiduminium-39
Decoltal-500
QQ-A-225/3Aluminium 2000 / Aluminium 2014A /2014 Aluminum Aluminium 2000 / Aluminium 2014A /2014 Aluminum Technical Data SheetAluminium 2000 / Aluminium 2014A /2014 Aluminum Chemical Composition LimitsWeight%AlSiFeCuMnCrMgNiZnTi+ZrTiOther EachOther Total2014a AECMARem0.50 - 0.900.50 max3.9 - 5.00.4-1.20.10 max0.2-0.80.1 max0.25 max0.20 max0.15 max0.05 max0.15 max2014 USARem0.50-1.200.7 max3.9 - 5.00.4 - 1.20.10 max0.2-0.8-0.25 max-0.15 max0.05 max0.15 maxAluminium Alloy 2014 (2014 A) is a copper based alloy with very high strength together with excellent machining characteristics. Alloy 2014 is commonly used in many aerospace structural applications due to its high strength. Other applications include military vehicles, bridges, weapons manufacture and structural applications.Aluminium 2000 / Aluminium 2014A /2014 Aluminum Mechanical PropertiesMaterialTemperThickness (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation in 50 mm0.5 mm0.8 mm1.3 mm2.6 mm3.0 mm2014 SheetT4 Bare0.2-6. SheetT6 Bare0.2-6. SheetT4 Clad0.2-1. SheetT4 Clad1.6-6. SheetT6 Clad0.2-1. SheetT6 Clad1.6-6.MaterialTemperDiameter (mm)Tensile Strength min ((N/mm²)Yield Strength (min) (N/mm²)Elongation on 5.65 V (min)2014 BarT4< BarT BarT BarT BarT BarT BarTAluminium 2000 / Aluminium 2014A /2014 Aluminum Specifications UNS A92014
Werkstoff Nr. 3.1255
Werkstoff Nr. 3.1254
AMS 4028 Sheet and Plate - Alloy 2014 T0
AMS 4029 Sheet and Plate - Alloy 2014 T651
AMS 4121 Bars, Rods, Wire (rolled or cold finished) - Alloy 2014 T6
AMS 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4134 Die Forgings - Alloy 2014 T4
AMS 4135 Superseded by 4133 Forgings, Rolled Rings - Alloy 2014 T6
AMS 4153 Extrusions - Alloy 2014 T6
BS 7L37 Rivet Stock
BS 3L63 Tube BS 2L77 Forging Stock T6 Temper BS 2L87 Bars and Sections T6 Temper BS 2L93 Plate Alloy 2014A BS L102 Bars and Sections T4 Temper BS L103 Forging Stock T4 Temper BS L105 Tube T4 Temper S07-1011, S07-1012 BS L156 Sheet and Strip T4 Temper BS L157 Sheet and Strip T6 Temper BS L158 Sheet and Strip T4 Temper Close Tolerance. BS L159 Sheet and Strip T6 Temper Close Tolerance. BS L163 Clad Sheet and Strip T3 Temper BS L163 Clad Sheet and Strip T4 Temper BS L164 Clad Sheet and Strip BS L165 Clad Sheet and Strip T6 Temper BS L166 Clad Sheet and Strip T4 Temper Close Tolerance. BS L167 Clad Sheet and Strip T6 Temper close Tolerance. BS L168 Bars and Sections T6, T6510 and T6511
BS H15, HS15, HP15, HT15, HE15.
AlCu4SiMg
A-U4SG
QQ-A-200/2
QQ-A-225/4
QQ-A-250/3
DTD 5010, Alloy 2014A
DTD 5030, DTD 5040
EN 2087
EN 2088
EN 2089 SHEET
EN 2395 SHEET
EN 2100 BAR T4511, EN 2634 BAR T4511
EN 2324 BAR, EN 2639 BAR, EN 2384, EN2635 T6, T6511
EN 2634 (with peripheral coarse grain control)
EN 2639 (with peripheral coarse grain control)
EN 2635 (with peripheral coarse grain control)
AECMA 2387Aluminium 2000 / Aluminium 2014A /2014 Aluminum Similar Specification
BS H15
Alcan GB-26S
AWCO-305
Birmetal-478
BA 305 and BA 355
Durcilium-K
Hiduminium-66
Avional-660 and Avional-662
BAEM 0039, BAEM 0128 and BAEM 0173
MIL-A-12545 Aluminium 2000 / Aluminium Alloy 2017A Aluminium 2000 / Aluminium Alloy 2017A Technical Data SheetAluminium 2000 / Aluminium Alloy 2017A Chemical Composition LimitsWeight%AlSiFeCuMnMgCrZnTiOthers EachOther Total2017 USARem0.20-0.80.7 max3.5-4.50.40-1.00.40-0.80.10 max0.25 max0.15 max0.05 max0.15 maxWeight%AlSiFeCuMnMgCrZnZr + TiOthers EachOther Total2017A EAARem0.20-0.80.7 max3.5-4.50.40-1.00.40-1.00.10 max0.25 max0.25 max0.05 max0.15 maxAluminium Alloy 2017 (2017 A) has high strength with excellent fatigue strength. Alloy 2017 also has very good machining characteristics. It is suitable for welding only by resistance welding. Alloy 2017 (2017 A) is used for various applications from high strength structural components, aircraft, machine construction, military equipment, rivets.Aluminium 2000 / Aluminium Alloy 2017A Mechanical PropertiesMaterialConditionTensile Strength (N/mm²) minYield StrengthElongation in 4D %ksiMpaksiMpa20172017-T4 BarAluminium 2000 / Aluminium Alloy 2017A Specifications
UNS A92017
Werkstoff Nr. 3.1325
ASTM B211 and ASTM B316
FED QQ-A-225/5 Bar, Rod and Wire
FED QQ-A-430 Wire and Rivets
AMS 4118 Bar, Rod and Wire 2017-T4 cold finished
AIR 9051AAluminium 2000 / Aluminium Alloy 2024 (2024A) Aluminium 2000 / Aluminium Alloy 2024 (2024A) Technical Data SheetAluminium 2000 / Aluminium Alloy 2024 (2024A) Chemical Composition LimitsWeight%SiFeCuMnMgCrZnTiOther EachOther TotalAl2024 USA0.50 max0.50 max3.8-4.90.3-0.91.2-1.80.10 max0.25 max0.15 max0.05 max0.15 maxRem2024A France0.15 max0.20 max3.7-4.50.15-0.81.2-1.50.10 max0.25 max0.15 max0.05 max0.15 maxRemAluminium 2024 (2024A) is one of the most popular high strength Aluminium alloys when it is the heat treated condition. Due to 2024 (2024A) high strength and excellent fatigue resistance it is commonly used on structures and components in the aircraft and transportation industries. Aluminium 2000 / Aluminium Alloy 2024 (2024A) SpecificationsAluminium 2000 / Aluminium Alloy 2024 (2024A) SpecificationsExtrustions /Part Numbers BS L97 Plate T351
BS L98 Plate T4
BS L109 Clad Sheet T4
BS L110 Clad Sheet T42
DTD 5100
WS 3.1354, BARE
WS 3.1364, ALCLAD
WS 3.1355
AMS 4033 Plate T351
AMS 4034 Plate Clad T351
AMS 4035 Sheet T0
AMS 4036 Sheet T3 Clad One Side, Plate T351
AMS 4037 Sheet T3, Plate T351
AMS 4040 Sheet T0 Clad
AMS 4041 Sheet T3 and T351 Clad Plate
AMS 4088 Tube T3 Drawn
AMS 4112 Wire rod / Bar Cold Finished T6
AMS 4119 Wire rod / Bar Cold Finished T351
AMS 4120 Wire rod / Bar Cold Finished T4
AMS 4152 Extruded Wire / Rod / Bar / Shapes T3
AMS 4165 Extruded Wire / Rod / Bar / Shapes T3511
FED QQ-A200/3
FED QQ-A225/6
FED QQ-A 250/4 SHEET
FED QQ-A 250/5 CLAD SHEET
MIL-T-50777 Seamless Tube
MIL-A-81596 Foil
QQ-A-200/3 2024 Extruded Rod, Bar, Shapes, tube and Wire
QQ-A-225/6 2024 Rolled, Drawn, Cold Finished Wire Rod and Bar
QQ-A-250/4 2024 Sheet and Plate O , T351, T851
QQ-A-250/5 2024 Alclad Sheet and Plate O, T3.
WW-T-700/3 2024 Drawn Seamless Tube
British Aerospace S071009
AIRBUS - ABM1-1005
BAEM 0145 and BAEM 0172
AIR 9048.630
AIR 9048.100
AIR 9048.110
AIR 9048.120
AIR 9048.130 Clad Sheet
AIR 9048.140 Clad Sheet
AIR 9049
AIR 9051A
AECMA 2710
EN 4101 T4 FORMING QUALITY
EN 2090 CLAD SHEET
EN 2091 CLAD SHEET
EN 2419 T351
EN2321 BAR
EN2318 BAR
EN 2638 (with peripheral coarse grain control)
EN 2633 (with peripheral coarse grain control)
EN 2703 CLAD SHEET
EN 3447 (with peripheral coarse grain control)
EN 3474
EN 3550 BAR
EN 3997
EN 3998
EN 3999
EN 4001 CLAD SHEET
EN 4101
EN 6000
ASN-A-3001 T351
ASN-A 3010 SHEET
ASN-A 3012
ASN-A 3058 Bar
ASN-A 3351
ASN-A 3048
CCT LA279
NCT 10-235-03MD
NCT 15-235-06MB
NCT 15-235-07MBAluminium 2000 / Aluminium Alloy 2031 Aluminium 2000 / Aluminium Alloy 2031 Technical Data SheetAluminium 2000 / Aluminium Alloy 2031 Chemical Composition LimitsWeight%SiFeCuMnMgNiZnTiOthers20310.50 / 1.30.60 / 1.21.8 / 2.80.50 max0.6 / 1.20.6 / 1.40.20 max0.20 max0.05 each
0.15 totalAluminium 2000 / Aluminium Alloy 2031 Mechanical PropertiesMaterialTemperCondition of sampleSize of Bar (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation on 5.65v2031 ForgingsTBForged< ForgingsTBExtruded< ForgingsTFForged< ForgingsTFExtruded<2003852856Aluminium 2000 / Aluminium Alloy 2031 Specifications
BS H12
Alcan GB-D15S
BA 307
Hiduminium-56Aluminium 2000 / Aluminium Alloy 2219 (AMS 4162 / AMS 4094) Aluminium 2000 / Aluminium Alloy 2219 Technical Data SheetAluminium 2000 / Aluminium Alloy 2219 Chemical Composition LimitsWeight%AlSiFeCuMnMgZnTiOthersVZn2219Bal0.20 max0.30 max5.80-6.800.20-0.400.02 max0.10 max0.02-0.100.050 each
0.15 total0.05-0.150.10-0.25Aluminium Alloy 2219 is a high strength alloy which combines good machinability and good mechanical properties. 2219 is useful over a temperature range of -452°F to 600°F, is readily weldable and has good fracture toughness. In the T8 condition it is resistant to stress corrosion cracking. Aluminium 2219 is typically used in a range of aerospace applications such as high temperature structural applications including space booster and fuel tanks.Aluminium 2000 / Aluminium Alloy 2219 Mechanical Properties Aluminium 2000 / Aluminium Alloy 2219 - Bar / ExtrusionsMaterialTemperDirectionTensile Strength ksiYield Strength ksiElongation in 2" (%)2219 (AMS 4162)T8511L584262219 (AMS 4162)T8511LT56394Aluminium 2000 / Aluminium Alloy 2219 - Sheet / Plater (Bare)MaterialTemperThicknessTensile Strength ksiYield Strength ksiElongation in 2" (%)2219 (QQ-A-250/30)00.020"-2.0032 max16 max122219 (QQ-A-250/30)T3510.250" - 2.00"4628102219 (QQ-A-250/30)T8510.250" - 2.00"62467-8Aluminium 2000 / Aluminium Alloy 2219- Sheet / Plater (Clad) Temper T81 / T851MaterialTemperThicknessTensile Strength ksiYield Strength ksiElongation in 2" (%)2219 (AMS 4094)T81/ T8510.020"-0.039"493762219 (AMS 4094)T81/ T8510.039"-0.099"554172219 (AMS 4094)T81/ T8510.099"-0.249"584372219 (AMS 4094)T81/ T8510.245"-0.499"58428Aluminium 2000 / Aluminium Alloy 2219 Specifications
AMS 4031 - 2219-0/F Sheet, Plate
AMS 4066 - 2219-T8511 Drawn, Seamless Tubing
AMS 4068 - 2219-T3511 Drawn, Seamless Tubing
AMS 4094 - 2219 T81 Clad Sheet / T851 Clad Plate
AMS 4095 - 2219 T31 Clad Sheet / T351 Clad Plate
AMS 4096 - 2219-0 Clad Sheet / Plate
AMS 4143 - 2219-T6 Forgings / Rolled or Forged Rings
AMS 4144 - 2219-T852/T851 Hand Forgings
AMS 4162 - 2219-T8511 Extrusions
AMS 4313 - 2219-T351/T352 Forgings/Rolled or forged rings
DMS1719 - 2219 T81 Alclad Sheet
QQ-A-250/30 - 2219 Bare Sheet, Plate
QQ-A-367
QQ-A-430
MIL-A-22771
MIL-A-46118
ASTM B209
ASTM B211
ASTM B221
ASTM B241
ASTM B316Aluminium 2000 / Aluminium Alloy 2618A (Aluminum 2618) Aluminium 2000 / Aluminium Alloy 2618A Technical Data SheetAluminium 2000 / Aluminium Alloy 2618A Chemical Composition LimitsWeight%AlSiFeCuMnMgNiZnTiZr + TiOther EachOthers Total2618 USARem0.10-0.250.9-1.31.9-2.7-1.3-1.80.9-1.20.10 max0.04-0.10-0.05 max0.15 max2618A EAARem0.15-0.250.9-1.41.8-2.70.25 max1.2-1.80.8-1.40.15 max0.20 max0.25 max0.05 max0.15 maxAluminium Alloy 2618A (Aluminum 2618) is a high strength aluminium alloy which contains both copper and magnesium. Alloy 2618 (2618A) has good machinability and is fair resistance to atmospheric attack. Aluminium Alloy 2618A (Aluminum 2618) is typically used in aerospace and defence components. It is commonly used for pistons and rotating aircraft parts due to it's ability to work in higher temperature applications. 2618 is also used in high performance autosport applications.Aluminium 2000 / Aluminium Alloy 2618A Mechanical PropertiesMaterialSizeDiameter (mm)Tensile Strength min (N/mm²)Yield Strength min (N/mm²)Elongation in 50 mm %2618AExtruded Bar