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Read MoreAluminium Alloy 2000 Series Stockist in India
Leading Aluminium Alloy 2011 Stockist in Mumbai, India. Aluminium 2014A/2219 Round Bars Supplier, AMS 4028 Aluminium 2017 Sheets Dealer, AMS 4033 Aluminium 2031 Plates Stockist. Reliable Aerospace Grade Aluminium Alloy 2000 Series Stockist & Exporter.
Aluminium 2000 Series alloys are copper-based aluminum alloys known for their high strength, excellent machinability, and good fatigue resistance. With superior mechanical properties and moderate corrosion resistance, these alloys are widely used in aerospace and defense applications where weight reduction, structural integrity, and high performance are critical. Common applications include aircraft structural components, aerospace fasteners, and defense-grade machinery where reliability and long-term durability are essential.
Aluminium Alloy 2000 Series
At Bhansali AeroAlloys, we supply premium-quality Aluminium Alloy 2000 Series round bars, sheets, plates, and custom forms engineered to meet the stringent requirements of aerospace and defense industries. Our commitment to precision, strict quality control, and timely delivery ensures materials that perform reliably in mission-critical applications. For technical guidance, custom solutions, or pricing inquiries, contact our expert team today at sales@bhansaliaeroalloys.com and partner with a trusted supplier of high-performance aluminum alloys.
Specifications For Aluminium Alloy 2000 Series
| Forms | Available in Round Bars, Sheets & Plates, Pipes (Custom Form Available) |
| Sizes | As per requirement |
| Applications | Aerospace Structural Applications, Aircraft Frames, Wings, Fuselage, Fuel Tanks, Armored Vehicles, Missiles, Defense-Grade Parts, etc. |
Aluminium Alloy 2000 Series
| Alloy Designation | UK Specifications | US Specifications | US Federal Specifications | European Specifications | Other |
|---|---|---|---|---|---|
| 2011 A92011 |
BS FC1 2011 Bar & Rod | QQ-A-225/3 2011 Bar, cold drawn | WS 3.1655 | AlCu(Bi/Mg)Pb A-U5PbBi |
|
| 2014A A92014 |
BS 7 L37 2014A Rivet stock BS 3 L63 2014A-T6 tube BS 2 L77 2014A Forging stock BS 2 L87 2014A-T6 Bar BS 2 L93 2014A-T651 Plate BS L102 2014A-T4 Bar BS L103 2014A-T4 Forging Stock BS L105 2014A-T4 Drawn tube BS L156 2014A-T4 Bare Sheet BS L157 2014A-T6 Bare Sheet BS L158 2014A-T4 Bare Sheet, close tolerance BS L159 2014A-T6 Bare Sheet, close tolerance BS L163 2014A-T3 Clad Sheet BS L164 2014A-T4 Clad Sheet BS L165 2014A-T6 Clad Sheet BS L166 2014A-T4 Clad Sheet, close tolerance BS L167 2014A-T6 Clad Sheet, close tolerance BS L168 2014A-T6 / T6511 Bar DTD 5010 Plate DTD 5030 Clad plate DTD 5040 Clad plate BS H15, HS15, HP15, HT15, HE15 |
AMS 4028 2014-T0 Sheet/Plate AMS 4029 2014-T651 Sheet/Plate AMS 4121 2014-T6/T6511 Bar AMS 4133 2014-T6 Forging AMS 4134 2014-T6 Die Forging AMS 4153 2014-T6 Extrusions |
QQ-A-200/2 2014-T4 Extruded bar QQ-A-200/2 2014-T6 Extruded bar QQ-A-225/4 2014-T4 Cold finished bar QQ-A-225/4 2014-T6 Cold finished bar QQ-A-250/3 2014-T4 Clad sheet QQ-A-250/3 2014-T6 Clad sheet QQ-A-367 MIL-A-21180 |
WS 3.1255 EN 2087 2014A-T6 Clad sheet EN 2088 2014A-T4 Clad sheet EN 2089 2014A-T6 Sheet EN 2100 2014A-T4511 Extruded bar EN 2324 2014A-T6 EN 2384 2014A-T6511 Extruded bar EN 2395 2014A-T4 Sheet EN 2634 2014A-T4511 Extruded bar EN 2635 2014A-T6511 Extruded bar, coarse grain control EN 2639 2014A-T6 |
A-U4SG AlCu4SiMg AECMA 2387 |
| 2017A A92017 |
AMS 4110 2017-451 (see AMS 4118) AMS 4118 2017-T4/T451 Bar |
QQ-A-225/5 Alloy 2017a | |||
| 2024 A92024 |
BS 2 L97 2024-T351 Plate BS 2 L98 2024-T4 Plate BS L109 2024-T4 Clad sheet BS L110 2024-F Clad sheet British Aerospace S071009 DTD 5100A Clad plate |
AMS 4033 2024-T351 AMS 4034 2024-T351 AMS 4035 2024-T0 Sheet/Plate AMS 4036 2024-T3/T351 Sheet (Alclad one side) AMS 4037 2024-T3/T351 Sheet/Plate AMS 4040 2024-T0 Alclad sheet/plate AMS 4041 2024-T3/T351 Alclad sheet/plate AMS 4077 2024-T0 Alclad sheet/plate AMS 4086 2024-T3 Seamless, drawn Hydraulic Tube AMS 4087 2024-T0 Seamless tube AMS 4088 2024-T3 Seamless tube AMS 4112 2024-T6 (see AMS 4339) AMS 4119 2024-T351 (see AMS 4120) AMS 4120 2024-T4/T351 Bar, wire AMS 4152 2024-T3 Extrusions AMS 4164 2024-T3510 Extrusions AMS 4165 2024-T3511 Extrusions AMS 4193 2024-T861 Sheet/Plate AMS 4194 2024-T361 1-1.5% Alclad AMS 4195 2024-T861 1.5% Alclad AMS 4270 2024-T3 Alclad sheet AMS 4339 2024-T851 Bar/rod |
QQ-A-200/3 2024-T4 Extruded bar QQ-A-200/3 2024-T8 Extruded bar QQ-A-225/6 2024-T351 Cold finished bar QQ-A-225/6 2024-T4 Cold finished bar QQ-A-225/6 2024-T851 Cold finished bar QQ-A-250/4 2024-0 Sheet and Plate QQ-A-250/4 2024-T3 Sheet and Plate QQ-A-250/5 2024-0 Alclad sheet and plate QQ-A-250/5 2024-T3 Alclad sheet and plate WW-T-700/3 2024-T3 Seamless, drawn tube MIL-T-50777 Seamless Tube MIL-A-81596 Foil |
WS 3.1354 Bare sheet WS 3.1364 Alclad sheet WS 3.1355 EN 2090 2024-T3 Clad sheet EN 2091 Clad sheet EN 2318 2024-T3511 Extruded bar EN 2321 EN 2419 T351 EN 2633 2024-T3511 Extruded bar EN 2638 EN 2703 2024-T4 Clad sheet EN 3447 EN 3474 2024-T81 Sheet EN 3550 EN 3997 2024-T3 Sheet EN 3998 2024-T4 Sheet EN 3999 2024-T351 Sheet EN 4001 2024-T351 Clad sheet EN 4101 2024-T4 Sheet EN 6000 |
Airbus ABM1-1005 BAEM 0145 / BAEM 0172 A-U4G1 AIR 9048.630 AIR 9048.100 AIR 9048.110 AIR 9048.120 AIR 9048.130 AIR 9048.140 AIR 9049 AIR 9051A AECMA 2710 ASN-A-3001 ASN-A-3010 ASN-A-3012 ASN-A-3058 ASN-A-3351 ASN-A-3048 CCT VA279 NCT 10-235-03MD NCT 15-235-06MB NCT 15-235-07MB |
| 2031 | BS 2 L83 2031 Rivet stock BS H12 |
A-U2N | |||
| 2219 |
AMS 4031 2219-T0 Sheet/Plate AMS 4066 2219-T851 Seamless tube AMS 4068 2219-T351 Seamless tube AMS 4094 2219-T851 Alclad sheet AMS 4095 2219-T351 Alclad sheet AMS 4096 2219-T0 Alclad sheet AMS 4143 2219-T6 Forgings AMS 4144 2219-T851/T852 Hand Forgings AMS 4162 2219-T8511 Extrusion AMS 4163 2219-T3511 Extrusion |
QQ-A-250/30 2219-0 MIL-A-22771 |
|||
| 2618A |
BS H16 DTD 745A 2618A Forging stock DTD 5014 2618-T6511 bar DTD 5014A 2618-T6511 bar DTD 5070B 2618-TF Clad sheet DTD 717A 2618 A -T6 Forging Stock and Forgings DTD 5084A T6 Forging Stock and Forgings DTD 731B 2618 T6 Forging Stock and Forgings |
AMS 4132 2618-T61 Die & Hand forgings | A-U2GN |
Aluminium Alloy 2011
Technical Data Sheet
- Alloy 2011 Overview: Aluminium 2011 is a heat-treatable, high-strength alloy with excellent fatigue strength.
- Machinability: Offers outstanding free-machining characteristics, making it ideal for precision components.
- Copper Content: High copper content enhances machinability, making Alloy 2011 the preferred choice for aluminium machining.
- Applications: Commonly used for:
- Screws
- Bolts
- Fittings and nuts
- Automatic lathe and screw machine products
Chemical Composition Limits 2011
| Alloy | Al | Si | Fe | Cu | Zn | Bi | Pb | Others |
|---|---|---|---|---|---|---|---|---|
| Alloy 2011 | Bal | 0.40 max | 0.70 max | 5.0–6.0 | 0.30 max | 0.20–0.60 | 0.20–0.60 | 0.05 (each) 0.15 (total) |
Typical Mechanical Properties
| Material | Temps | Thickness (min) | Tensile Strength (N/mm²) min | Yield Strength (N/mm²) min | Elongation on 50mm (%) |
|---|---|---|---|---|---|
| Alloy 2011 Bar | TD | <10 | 310 | 255 | 6 |
| Alloy 2011 Bar | TD | 10–35 | 310 | 255 | 8 |
| Alloy 2011 Bar | TD | 35–50 | 295 | 230 | 8 |
| Alloy 2011 Bar | TF | <65 | 310 | 225 | 8 |
| Alloy 2011 Bar | TF | >65 | 295 | 195 | 8 |
Chemical Composition Limits 2014A
| Alloy | Al | Si | Fe | Cu | Mn | Cr | Mg | Ni | Zn | Ti+Zr | Ti | Other Each | Other Total |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Alloy 2014a AECMA | Rem | 0.50 - 0.90 | 0.50 max | 3.9 - 5.0 | 0.4 - 1.2 | 0.10 max | 0.2 - 0.8 | 0.1 max | 0.25 max | 0.20 max | 0.15 max | 0.05 max | 0.15 max |
| Alloy 2014 USA | Rem | 0.50 - 1.20 | 0.70 max | 3.9 - 5.0 | 0.4 - 1.2 | 0.10 max | 0.2 - 0.8 | - | 0.25 max | - | 0.15 max | 0.05 max | 0.15 max |
Typical Mechanical Properties
| Material | Temper | Thickness (mm) | Tensile Strength min (N/mm²) | Yield Strength min (N/mm²) | Elongation in 50 mm | ||||
|---|---|---|---|---|---|---|---|---|---|
| 0.5 mm | 0.8 mm | 1.3 mm | 2.6 mm | 3.0 mm | |||||
| Alloy 2014 Sheet | T4 Bare | 0.2-6.0 | 400 | 225 | 13 | 14 | 14 | 14 | 14 |
| Alloy 2014 Sheet | T6 Bare | 0.2-6.0 | 440 | 380 | 6 | 6 | 7 | 7 | 8 |
| Alloy 2014 Sheet | T4 Clad | 0.2-1.6 | 385 | 240 | 13 | 14 | 14 | - | - |
| Alloy 2014 Sheet | T4 Clad | 1.6-6.0 | 395 | 245 | - | - | - | 14 | 14 |
| Alloy 2014 Sheet | T6 Clad | 0.2-1.6 | 420 | 345 | 7 | 7 | 8 | - | - |
| Alloy 2014 Sheet | T6 Clad | 1.6-6.0 | 420 | 355 | - | - | - | 9 | 9 |
| Material | Temper | Diameter (mm) | Tensile Strength min (N/mm²) | Yield Strength min (N/mm²) | Elongation on 5.65√S₀ (min) |
|---|---|---|---|---|---|
| Alloy 2014 Bar | T4 | <20 | 370 | 230 | 11 |
| Alloy 2014 Bar | T4 | 20-75 | 390 | 250 | 11 |
| Alloy 2014 Bar | T4 | 75-150 | 390 | 250 | 9 |
| Alloy 2014 Bar | T4 | 150-200 | 370 | 230 | 8 |
| Alloy 2014 Bar | T6510 | 20-75 | 480 | 435 | 7 |
| Alloy 2014 Bar | T6510 | 75-150 | 465 | 420 | 7 |
| Alloy 2014 Bar | T6510 | 150-200 | 435 | 390 | 7 |
Chemical Composition Limits 2017
| Weight% | Al | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti / Zr + Ti | Others Each | Other Total |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Alloy 2017 USA | Rem | 0.20-0.8 | 0.7 max | 3.5-4.5 | 0.40-1.0 | 0.40-0.8 | 0.10 max | 0.25 max | 0.15 max | 0.05 max | 0.15 max |
| Weight% | Al | Si | Fe | Cu | Mn | Mg | Cr | Zn | Zr + Ti | Others Each | Other Total |
| Alloy 2017A EAA | Rem | 0.20-0.8 | 0.7 max | 3.5-4.5 | 0.40-1.0 | 0.40-1.0 | 0.10 max | 0.25 max | 0.25 max | 0.05 max | 0.15 max |
Typical Mechanical Properties
| Material | Condition | Tensile Strength (min) | Yield Strength | Elongation in 4D % | ||
|---|---|---|---|---|---|---|
| ksi | MPa | ksi | MPa | |||
| Alloy 2017 | 2017-T4 Bar | 55 | 379 | 32 | 221 | 12 |
Chemical Composition Limits 2024
| Weight% | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Other Each | Other Total | Al |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Alloy 2024 USA | 0.50 max | 0.50 max | 3.8-4.9 | 0.3-0.9 | 1.2-1.8 | 0.10 max | 0.25 max | 0.15 max | 0.05 max | 0.15 max | Rem |
| Alloy 2024A France | 0.15 max | 0.20 max | 3.7-4.5 | 0.15-0.8 | 1.2-1.5 | 0.10 max | 0.25 max | 0.15 max | 0.05 max | 0.15 max | Rem |
Chemical Composition Limits 2031
| Weight% | Si | Fe | Cu | Mn | Mg | Ni | Zn | Ti | Others |
|---|---|---|---|---|---|---|---|---|---|
| Alloy 2031 | 0.50 / 1.3 | 0.60 / 1.2 | 1.8 / 2.8 | 0.50 max | 0.6 / 1.2 | 0.6 / 1.4 | 0.20 max | 0.20 max | 0.05 each 0.15 total |
Typical Mechanical Properties
| Material | Temper | Condition of Sample | Size of Bar (mm) | Tensile Strength min (N/mm²) | Yield Strength min (N/mm²) | Elongation on 5.65v |
|---|---|---|---|---|---|---|
| Alloy 2031 Forgings | TB | Forged | <150 | 310 | 160 | 13 |
| Alloy 2031 Forgings | TB | Extruded | <200 | 310 | 145 | 13 |
| Alloy 2031 Forgings | TF | Forged | <150 | 385 | 300 | 6 |
| Alloy 2031 Forgings | TF | Extruded | <200 | 385 | 285 | 6 |
Chemical Composition Limits 2219
| Weight% | Al | Si | Fe | Cu | Mn | Mg | Zn | Ti | Others | V | Zn |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Alloy 2219 | Bal | 0.20 max | 0.30 max | 5.80-6.80 | 0.20-0.40 | 0.02 max | 0.10 max | 0.02-0.10 | 0.050 each 0.15 total |
0.05-0.15 | 0.10-0.25 |
Typical Mechanical Properties
| Material | Temper | Direction | Tensile Strength (ksi) | Yield Strength (ksi) | Elongation in 2" (%) |
|---|---|---|---|---|---|
| Alloy 2219 (AMS 4162) | T8511 | L | 58 | 42 | 6 |
| Alloy 2219 (AMS 4162) | T8511 | LT | 56 | 39 | 4 |
| Material | Temper | Thickness | Tensile Strength (ksi) | Yield Strength (ksi) | Elongation in 2" (%) |
|---|---|---|---|---|---|
| Alloy 2219 (QQ-A-250/30) | 0 | 0.020" - 2.00" | 32 max | 16 max | 12 |
| Alloy 2219 (QQ-A-250/30) | T351 | 0.250" - 2.00" | 46 | 28 | 10 |
| Alloy 2219 (QQ-A-250/30) | T851 | 0.250" - 2.00" | 62 | 46 | 7-8 |
| Material | Temper | Thickness | Tensile Strength (ksi) | Yield Strength (ksi) | Elongation in 2" (%) |
|---|---|---|---|---|---|
| Alloy 2219 (AMS 4094) | T81/ T851 | 0.020" - 0.039" | 49 | 37 | 6 |
| Alloy 2219 (AMS 4094) | T81/ T851 | 0.039" - 0.099" | 55 | 41 | 7 |
| Alloy 2219 (AMS 4094) | T81/ T851 | 0.099" - 0.249" | 58 | 43 | 7 |
| Alloy 2219 (AMS 4094) | T81/ T851 | 0.245" - 0.499" | 58 | 42 | 8 |
Chemical Composition Limits 2618A
| Weight% | Al | Si | Fe | Cu | Mn | Mg | Ni | Zn | Ti | Zr + Ti | Other Each | Others Total |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Alloy 2618 USA | Rem | 0.10-0.25 | 0.9-1.3 | 1.9-2.7 | - | 1.3-1.8 | 0.9-1.2 | 0.10 max | 0.04-0.10 | - | 0.05 max | 0.15 max |
| Alloy 2618A EAA | Rem | 0.15-0.25 | 0.9-1.4 | 1.8-2.7 | 0.25 max | 1.2-1.8 | 0.8-1.4 | 0.15 max | 0.20 max | 0.25 max | 0.05 max | 0.15 max |
Typical Mechanical Properties
| Material | Size | Diameter (mm) | Tensile Strength min (N/mm²) | Yield Strength min (N/mm²) | Elongation in 50 mm % |
|---|---|---|---|---|---|
| Alloy 2618A | Extruded Bar | <10 | 400 | 320 | 5 |
| Alloy 2618 | Extruded Bar | 10-100 | 420 | 340 | 7 |
