Why Chalco 5056 truc tiep bong da anh wire?
Quality could full meet worldwide aviation standard
BS 3 L58 Alloy 5056 A Rivet Stock
AMS 4182 5056-O Wire
QQ-A-430 5056-O Rivet wire
We meet international aviation quality certification standards
AS9100
OHSAS 18001
ISO14001
ISO 9001
NADCAP HT
NADCAP NDT
IATP16949
Chalco is a manufacturer with advanced technology and R&D capabilities in the field of aerospace materials, committed to common development with customers.
Specification and application for 5056 truc tiep bong da anh wire
| Specification (Diameter) | Application |
| 3/32 inch (2.38 mm) | Small riveting, such as thin sheet metal and truc tiep bong da anh parts |
| 1/8 inch (3.18 mm) | Suitable for general-purpose riveting |
| 5/32 inch (3.97 mm) | Large riveting, such as aircraft shells |
| 3/16 inch (4.76 mm) | Large riveting, such as aircraft shells and wings |
Chemical composition for 5056 truc tiep bong da anh wire
| Element | Composition(%) |
| truc tiep bong da anh (Al) | Balance |
| Copper (Cu) | 4.5-5.6% |
| Magnesium (Mg) | 0.6-1.6% |
| Manganese (Mn) | 0.4-1.0% |
| Chromium (Cr) | 0.05-0.25% |
| Zirconium (Zr) | 0.08-0.2% |
| Titanium (Ti) | 0.15-0.4% |
| Silicon (Si) | ≤0.40% |
| Iron (Fe) | ≤0.5% |
| Tin (Sn) | ≤0.2% |
| Other | ≤0.15% |
Mechanical properties for 5056 aluminium wire
| Tensile strength | 345 MPa |
| Yield strength | 265 MPa |
| Elongation (BS 3 L58) | 8% |
| Elongation (QQ-A-430 and AMS 4182) | 10% |
What are the characteristics of Chalco 5056 aviation truc tiep bong da anh wire?
Good surface quality
- Surface flatness: the surface should be smooth and flat, without significant protrusions or depressions.
- Surface cleanliness: the surface should be free from impurities such as oil, dust, and oxide scale.
Good processing properties
- Good plasticity suitable for deep drawing;
- Good weldability suitable for various welding methods;
- Good machinability suitable for various cutting and drilling operations.
Light weight
Compared with other metal materials, truc tiep bong da anh alloy has a lower density, which can reduce the weight of the structure and help improve the fuel efficiency and load capacity of the aircraft.
