Xi'an Dongmeng Group Co., Ltd. is one of the most reliable manufacturers and suppliers of 7050 Aluminum Alloy Plate Sheet Bar | Aerospace Grade 7050 T7451 T7651 Aluminum Supplier Manufacturer in China, also supports customized service. With abundant experience, we warmly welcome you to wholesale cheap products in stock here and get free sample from our factory. For price consultation, contact us.
Aluminum Alloy 7050 (also known as 7050 aluminum plate, 7050 aluminum sheet, 7050 aluminum bar, 7050 aerospace alloy) is a premium high-strength aluminum-zinc-magnesium-copper alloy widely used in aerospace structural components. Known for its exceptional toughness, outstanding stress corrosion cracking resistance, high fatigue strength, and excellent hardenability, 7050 alloy is preferred for thick cross-sections in aircraft and defense engineering.
Our factory supplies 7050-T7451/T7651 plates, 7050-T6/T651 sheets, 7050-T73/T74 bars, and precision-machined parts, with full export packaging, mill certificates, and global shipping support.

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High Quality
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Advanced Equipment
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Professional Team
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Custom Service
What Is 7050 Aluminum Alloy?
7050 aluminum alloy is a high-strength heat-treatable wrought aluminum alloy primarily developed for aerospace structural applications requiring exceptional mechanical strength, fracture toughness, and resistance to stress corrosion cracking.
Compared with conventional 7075 aluminum alloy, 7050 aluminum plate offers:
Better stress corrosion resistance
Improved thick-section performance
Superior fracture toughness
Enhanced fatigue resistance
Better structural stability under high-load environments
Because of these advantages, 7050 T7451 aluminum plate is widely used in:
Aircraft wing structures
Aerospace bulkheads
Fuselage frames
Military structural components
Precision CNC aerospace machining
Xi'an Dongmeng Group Co., Ltd specializes in manufacturing export-grade 7050 aerospace aluminum alloy products with strict dimensional tolerances, full traceability, and international standard compliance.
Chemical Composition (Typical %)
| Element | Content (%) |
|---|---|
| Zinc (Zn) | 5.7 – 6.7 |
| Magnesium (Mg) | 1.9 – 2.6 |
| Copper (Cu) | 2.0 – 2.6 |
| Zirconium (Zr) | 0.08 – 0.15 |
| Iron (Fe) | ≤ 0.15 |
| Silicon (Si) | ≤ 0.12 |
| Manganese (Mn) | ≤ 0.10 |
| Titanium (Ti) | ≤ 0.06 |
| Others | ≤ 0.05 each |
| Aluminum (Al) | Balance |
Mechanical Properties
| Property | 7075-T6 | 7075-T651 | 7075-T73 | 7075-T74 |
|---|---|---|---|---|
| Tensile Strength (MPa) | 572 | 572 | 505 | 510 |
| Yield Strength (0.2% MPa) | 503 | 503 | 435 | 441 |
| Elongation (%) | 11 | 11 | 13 | 13 |
| Hardness (HB) | 150 | 150 | 135 | 140 |
| Fatigue Strength (MPa) | 160 | 160 | 155 | 158 |
| Shear Strength (MPa) | 331 | 331 | 295 | 300 |
| Modulus of Elasticity (GPa) | 71.7 | 71.7 | 71.7 | 71.7 |
| Density (g/cm³) | 2.81 | 2.81 | 2.81 | 2.81 |
Physical Properties
| Property | Value |
|---|---|
| Density | 2.83 g/cm³ |
| Melting Point | 477 – 635°C |
| Thermal Conductivity | 130 W/m·K |
| Electrical Conductivity | 35% IACS |
| Elastic Modulus | 71 GPa |
Aluminum Alloy 7075 – Product Specifications
1. 7075 Aluminum Plate (T651 / T7451 / T7651)
| Thickness (mm) | Thickness (inch) | Width (mm) | Width (inch) | Length (mm) | Length (feet) | Tolerance |
|---|---|---|---|---|---|---|
| 6 – 10 | 0.24 – 0.39 | 1000–2500 | 39–98 | 2000–6000 | 6.5–20 ft | ASTM B209 |
| 12 – 25 | 0.47 – 0.98 | 1000–2500 | 39–98 | 2000–6000 | 6.5–20 ft | ASTM B209 |
| 30 – 80 | 1.18 – 3.15 | 1000–2500 | 39–98 | 2000–6000 | 6.5–20 ft | ASTM B209 |
| 90 – 150 | 3.54 – 5.91 | 1000–2500 | 39–98 | 2000–6000 | 6.5–20 ft | ASTM B209 |
| 160 – 300 | 6.30 – 11.8 | 1000–2500 | 39–98 | 2000–6000 | 6.5–20 ft | Customized |
2. 7075 Aluminum Sheet (T6 / T651)
| Thickness | Metric (mm) | Imperial (inch) | Width | Length |
|---|---|---|---|---|
| Thin Sheet | 0.4 – 3.0 | 0.016 – 0.12 | 500–1500 mm | 1000–4000 mm |
| Medium Sheet | 3.0 – 6.0 | 0.12 – 0.24 | 500–1500 mm | 1000–4000 mm |
3. 7075 Aluminum Round Bar / Rod
| Diameter (mm) | Diameter (inch) | Length (mm) | Length (feet) | Tolerance (ASTM B211) |
|---|---|---|---|---|
| 6 – 20 | 0.24 – 0.79 | 2000–6000 | 6.5–20 ft | h9 / h10 |
| 22 – 80 | 0.87 – 3.15 | 2000–6000 | 6.5–20 ft | h10 |
| 90 – 200 | 3.54 – 7.87 | 2000–6000 | 6.5–20 ft | h11 |
| 210 – 300 | 8.27 – 11.8 | 2000–6000 | 6.5–20 ft | Customized |
4. 7075 Aluminum Square / Flat Bar
| Type | Size Range (mm) | Size Range (inch) | Length |
|---|---|---|---|
| Square Bar | 10×10 – 200×200 | 0.39×0.39 – 7.87×7.87 | 2–6 m |
| Flat Bar | 10×2 – 200×50 | 0.39×0.08 – 7.87×1.97 | 2–6 m |
5. 7075 Aluminum Tube (Extruded/Seamless)
| OD (mm) | OD (inch) | Wall Thickness (mm) | Wall Thickness (inch) | Standard |
|---|---|---|---|---|
| 10 – 200 | 0.39 – 7.87 | 1 – 25 | 0.04 – 1.0 | ASTM B241 |
| 210 – 300 | 8.27 – 11.8 | 5 – 30 | 0.20 – 1.18 | Customized |
6. Standard Compliance
ASTM B209 – Plates & Sheets
ASTM B211 – Bars & Rods
ASTM B221 – Extruded Products
ASTM B241 – Seamless Aluminum Tubes
AMS 4045, AMS 4078, AMS 4124
Machining Performance Analysis
CNC Machining Characteristics of 7050 Aluminum Alloy
7050 aluminum alloy demonstrates excellent machining behavior in aerospace CNC manufacturing environments. Due to its high structural strength and dimensional stability, it is ideal for precision-machined aircraft components.
Machining Advantages
Excellent chip control during high-speed machining
Stable dimensional tolerance performance
Reduced machining deformation
Good surface finish quality
Suitable for deep cavity aerospace parts
Typical CNC Machined Products
Aircraft ribs
Structural brackets
Wing fittings
Aerospace tooling plates
Precision defense components
Welding Performance Analysis
7050 aluminum alloy is generally not recommended for conventional fusion welding because of its susceptibility to hot cracking and reduced weld-zone strength.
For structural applications:
Mechanical fastening is preferred
Friction stir welding may be used in specialized applications
Aerospace structural assemblies typically rely on bolting or riveting systems
For customers requiring fabricated aerospace structures, Xi'an Dongmeng Group Co., Ltd can provide machining-ready semi-finished materials with optimized temper conditions.
Corrosion Resistance Analysis
Stress Corrosion Resistance of 7050 Aluminum Alloy
Compared with standard 7xxx aluminum alloys, 7050 T7451 aluminum offers significantly improved resistance to stress corrosion cracking.
This makes it highly suitable for:
Aircraft fuselage structures
Marine atmospheric environments
High-humidity operational conditions
Long-life aerospace systems
The alloy also provides:
Excellent exfoliation corrosion resistance
Stable long-term mechanical reliability
Superior fracture toughness in thick plates
Key Features & Advantages
Very high strength in thick sections
Superior toughness compared to 7075
Excellent stress corrosion cracking resistance
Outstanding fracture toughness
Good fatigue resistance
High hardenability for heavy cross-sections
Stable mechanical properties after heat treatment
Suitable for precision machining and aerospace structures
Industry Applications of 7050 Aluminum Alloy

Aerospace Industry
Applications
Aircraft wing skins
Bulkheads
Structural frames
Landing gear support structures
Fuselage reinforcements
Benefits
High strength-to-weight ratio
Excellent fatigue performance
Structural reliability
Long service life

Defense & Military Industry
Applications
Military aircraft structures
Armored support systems
Missile structural components
Defense machining parts
Benefits
High-load capability
Stable metallurgy
Impact resistance
Precision machining compatibility

High-Precision CNC Manufacturing
Applications
Aerospace tooling plates
Precision fixtures
High-speed machining blocks
Structural machining components
Benefits
Dimensional stability
Excellent machinability
Reduced deformation
High productivity
Inspection & Quality Assurance
We provide complete quality control throughout production:
100% UT ultrasonic testing (per AMS-STD-2154)
Chemical composition analysis using spectrometer
Mechanical property testing: tensile, hardness, yield
Grain size & fracture toughness inspection
Dimensional & surface inspection
Third-party inspection available (SGS / BV / TUV)
Mill Test Certificate (EN10204 3.1 / 3.2)
For quotations, samples, or technical datasheets, please contact our sales team:
Our address
Room 4107, Runfeng Building, Sanqiao New Street, Weiyang District, Xi'an City, Shaanxi Province
Phone Number
+86 15769214734

FAQ
Q1: What are the main advantages of Aluminum 7075?
7075 offers very high strength, excellent fatigue resistance, good machinability, and strong performance-to-weight ratio. It is one of the strongest commercial aluminum alloys, widely used in aerospace and high-load structural parts.
Q2: What is the difference between 7075-T6 and 7075-T651?
Both have similar strength, but T651 is stress-relieved by stretching, making it more stable for machining and preventing deformation in thick plates.
T6: sheet, bar
T651: plate (most common)
Q3: When should I choose T73 or T74 temper instead of T6/T651?
Use T73/T74 when your project requires superior stress corrosion cracking (SCC) and exfoliation corrosion resistance.
T73 has the best corrosion resistance, while T74 provides a balance of strength and SCC resistance.
Q4: What standards do you follow when supplying 7075 aluminum?
Common export-grade standards:
ASTM B209 (plates, sheets)
ASTM B211 (bars, rods)
ASTM B221 (extruded products)
AMS 4045 / AMS 4078 / AMS 4124
EN 485 / EN 573
Q5: Do you provide ultrasonic tested (UT) plates for aerospace use?
Yes. We supply 100% UT-tested 7075 plates according to AMS-STD-2154, Level A/B requirements.
Q6: What is the maximum thickness of 7075 plate you can supply?
We can supply 6–300 mm standard, and thicker customized sizes on request.
Q7: Can 7075 aluminum be welded?
7075 has poor weldability and typically is not recommended for fusion welding. Mechanical fastening or friction stir welding (FSW) is preferred in engineering applications.
Q8: What machining services are available?
We offer CNC milling, sawing, turning, surface machining, and customized shapes. T651 plates are widely used for precision machining due to high stability.
Q9: Do you provide MTC and third-party inspection?
Yes. We provide:
Mill Test Certificate (EN10204 3.1)
Chemical analysis
Mechanical properties
UT report
Third-party inspection: SGS / BV / TUV available.
Q10: What is your delivery time?
Stock items: 3–7 days
Customized cutting: 7–12 days
Special tempers / large-size forgings: 15–30 days
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