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2219 clad
AMS 4094 / AlCu6Mn / 2219 clad / T851
| Chemical Properties | % Value |
| Silicon (Si) | 0,00 - 0,20 |
| Manganese (Mn) | 0,20 - 0,40 |
| Magnesium (Mg) | 0,00 - 0,02 |
| Copper (Cu) | 5,80 - 6,80 |
| Titanium (Ti) | 0,02 - 0,10 |
| Iron (Fe) | 0,00 - 0,30 |
| Zinc (Zn) | 0,00 - 0,10 |
| Nickel (Ni) | 0,00 - 0,20 |
| Aluminium (Al) | Balance |
| Titanium + Zirconium (Ti+Zr) | 0,10 - 0,25 |
| Physical Properties | Value |
| Density | 2.84 g/cm³ |
| Melting Point | 543 °C |
| Thermal Expansion | 20.8 µm/m-°C |
| Modulus of Elasticity | 74 GPa |
| Thermal Conductivity | 120 W/m.K |
| Electrical Resistivity | 30% IACS |
| Mechanical Properties | Value |
| Proof Strength | 290 MPa |
| Yield Strength | 400 MPa |
| Shear Strength | 210 MPa |
| Elongation A50 mm | 8.0 % |
| Hardness | 130 HB |
| 2219 Clad T851 Temperature – Ultimate Tensile Strength Graph |
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| 2219 Clad T851 Thickness – Ultimate Tensile Strength Graph |
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| 2219 Clad T851 Diameter – Ultimate Tensile Strength Graph |
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2219 clad T851 aluminum alloy is distinguished by its high strength and excellent elevated temperature resistance, and it is widely used particularly in the aerospace industry. The T851 temper includes solution heat treatment, stress relieving, and artificial aging processes; this provides the alloy with high mechanical strength and dimensional stability. Thanks to its clad structure, a layer of purer aluminum exists on the surface, and this significantly improves corrosion resistance. Due to these features, it is preferred in fuel tanks, rocket structures, and cryogenic storage systems.
When evaluated in terms of corrosion resistance, 2219 clad T851 is much more advantageous compared to its unclad version. The pure aluminum cladding forms a protective barrier against environmental effects and oxidation. In terms of strength, its ability to maintain performance even at high temperatures makes it superior to alloys such as 2024-T3 and 7075-T6 in certain applications. Especially its ability to retain performance in the 150–250°C range makes this alloy critical in aerospace and defense industries.
In terms of machinability, 2219 alloy offers a moderate level of performance. Although it is not as easy to machine as 6061-T6, good results can be achieved with proper cutting parameters and tool selection. Its bending capability is limited; especially in the T851 temper, forming operations require attention due to high strength. Therefore, forming operations are generally carried out in softer tempers such as T4, followed by aging.
In terms of coatability and surface treatments, the clad structure already provides natural protection, reducing the need for additional coating; however, anodizing and other surface treatments can still be applied. In terms of vibration response, it exhibits stable behavior under vibration thanks to its high rigidity, making it reliable in structural applications. Its weldability is quite good, especially with TIG and MIG welding methods; this makes it a preferred alloy for large structural components.
Overall, 2219 clad T851 aluminum alloy stands out with its high temperature resistance, good weldability, and improved corrosion resistance. Compared to 2024, 7075, and 6061 alloys, each has different advantages; however, 2219 offers a unique balance especially in applications requiring high temperature and welding. Therefore, it is used as a critical material in advanced engineering fields such as aerospace, defense, and cryogenic systems.
2219 T851 clad can be produced according to the following standards:
• 2219 T851 Alclad Plate; ASTM B209, UNS A92219, ISO AlCu6Mn, AMS 4094
Selection Factors for 2219 T851 clad
- Strength: Excellent
- Machinability: Poor
- Weldability: Very Good
- Formability: Suitable
- Corrosion Resistance: Notable
- Heat Treatment: Yes
Common Applications for 2219 T851 clad
It is used in aircraft landing gear,
Bicycle frames and bridge components,
Rocket engine chassis, among many other applications.
2219 T851 clad is produced/supplied in sheet form.
- Sheet



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