Chalco produces and supplies 6013-T6 and 6013-T4 aviation aluminum alloy plates specified by AMS 4216 specification, which are widely used in the aerospace field, such as manufacturing wings, flaps, fuselage, engine covers and other parts.
Why choose Chalco AMS 4216 6013-T6/T4 aerospace aluminum sheet?
Chalco Aluminum provides excellent quality aerospace materials, as well as the best technical services in the market, and has a deep knowledge base on how to support customers in meeting the challenges of the future.
Quality could full meet aviation standard
A97050
AMS 4344
AMS 4341
AMS 4216 etc.
Chalco accreditation
We have passed AS9100, OHSAS 18001 and other certifications required by the aviation industry, providing a strong guarantee for the quality of aerospace materials produced by our company.
AS9100
OHSAS 18001
ISO14001
ISO9001
NADCAP HT
NADCAP NDT
IATP16949
Chemical composition of AMS 4216 6013-T6 and 6013-T4 aviation aluminum sheets
| Element | Composition | |
| 6013-T6 | 6013-T4 | |
| Si | 0.6-1.0% | 0.6-1.0% |
| Fe | 0.50% | 0.50% |
| Cu | 0.1-0.3% | 0.1-0.3% |
| Mn | 0.2-0.6% | 0.2-0.6% |
| Mg | 0.9-1.3% | 0.9-1.3% |
| Cr | 0.1-0.25% | 0.1-0.25% |
| Zn | 0.20% | 0.20% |
| Ti | - | - |
| Zr | - | - |
| Other (each) | 0.05% | 0.05% |
| Other (total) | 0.15% | 0.15% |
| Al | Remainder | Remainder |
Properties of AMS 4216 6013-T6 and 6013-T4 aviation aluminum sheets
| Temper | T6 | T4 |
| Density | 2.78 g/cm3 | 2.78 g/cm3 |
| Tensile strength | 470 MPa | 380 MPa |
| Yield strength | 390 MPa | 325 MPa |
| Elongation | 7% | 10% |
| Hardness (HB) | 130 | 100 |
| Bending strength | 600 MPa | 450 MPa |
| Fatigue strength | 150 MPa | 125 MPa |
| Coefficient of thermal expansion | 23.2*10-6/K | 23.2*10-6/K |
| Thermal conductivity | 130 W/(m·K) | 130 W/(m·K) |
| Conductivity | 35.2 MS/m | 35.2 MS/m |
Common dimensions of AMS 4216 6013-T6 and 6013-T4 aviation aluminum sheets
| Temper | Thickness | Width | Length |
| T6 | 0.0125-0.499" | 12.0-72.0" | 24.0-192.0" |
| T6 | 0.500-1.000" | 12.0-72.0" | 24.0-192.0" |
| T6 | 1.001-2.000" | 12.0-72.0" | 24.0-144.0" |
| T6 | 2.001-3.000" | 12.0-72.0" | 24.0-72.0" |
| T4 | 0.0125-0.499" | 12.0-72.0" | 24.0-192.0" |
| T4 | 0.500-1.000" | 12.0-72.0" | 24.0-192.0" |
| T4 | 1.001-2.000" | 12.0-72.0" | 24.0-144.0" |
| T4 | 2.001-3.000" | 12.0-72.0" | 24.0-72.0" |
Application of AMS 4216 6013-T6 and 6013-T4 aviation aluminum alloy plates
Aircraft structures: due to their high strength and lower density, 6013-T6 and 6013-T4 alloy sheets are commonly used to manufacture components in aircraft structures, such as airfoils, fuselages, leading edge panels, bulkheads, etc.
Engine covers: 6013-T6 and 6013-T4 alloy plates have high strength and hardness, making them ideal for parts such as aircraft engine covers.
Main characteristics of AMS 4216 6013-T6 and 6013-T4 aerospace aluminum alloy plates
Chemical composition: the main components of 6013-T6 and 6013-T4 alloy plates are aluminum, silicon, copper, magnesium and manganese, and the content of other elements is relatively low.
Physical properties: 6013-T6 alloy plate has high tensile strength and yield strength, and relatively high hardness, but low elongation. The 6013-T4 alloy plate has lower physical properties but higher elongation.
Heat treatment properties: 6013-T6 and 6013-T4 alloy plates can obtain the required mechanical properties and ductility through proper heat treatment. Heat treatment changes the physical properties of the alloy sheet to suit different application needs.
Corrosion resistance: 6013-T6 and 6013-T4 alloy plates have good corrosion resistance and can resist oxidation, corrosion and other environmental influences.
Machinability: 6013-T6 and 6013-T4 alloy plates have good machinability and can be processed by cutting, drilling, punching, forming and welding.
Precautions when using AMS 4216 6013-T6 and 6013-T4 aviation aluminum alloy plates
Confirm the standards and specifications of the alloy plate
Selecting the appropriate aviation aluminum plate needs to be based on specific application requirements, and confirm the standards and specifications of the alloy plate to ensure that it meets the required performance requirements.
Controlling processing and heat treatment process
The processing and heat treatment process of alloy plate may have an impact on its properties. In order to ensure that the alloy plate meets the required performance requirements, appropriate processing and heat treatment measures should be taken, and the process should be strictly controlled.
Avoid damage to the surface
The surface of the aviation aluminum sheet is susceptible to scratches and damage, which can lead to surface defects and corrosion. During storage and transportation, appropriate measures should be taken to avoid surface damage.
Ensure proper welding and joints
Aviation aluminum panels usually need to be joined by welding and joints. It is very important to ensure correct welds and joints to ensure the strength and stability of the joint.
Avoid contact with incompatible metals
The performance of aerospace aluminum panels may be affected by contact with incompatible metals. During the design and manufacturing process, the aviation aluminum plate should be avoided from contacting with incompatible metals to ensure its performance and reliability.
Strict control of environmental conditions
Aviation aluminum panels may be affected by environmental conditions, such as temperature, humidity and chemicals. During storage, transportation and use, appropriate measures should be taken to strictly control the environmental conditions to ensure the performance and reliability of aviation aluminum panels.
