7075-T651 Aluminum Plate

Aerospace grade 7075-T651 aluminum plate — ultra-high strength (572 MPa). Used in aircraft structures, defense, and high-performance tooling. Thickness 6-150mm. AMS 4045 compliant.

Temper T651 / T6 / T7351 Thickness 6 – 150 mm Strength 572 MPa
Temper
T651/T6
Stress relieved plate
Tensile Strength
572 MPa
Yield: 503 MPa
Thickness
6-150mm
Width up to 2500 mm
Hardness
150 HB
Brinell scale

Overview of 7075-T651 Aluminum Plate

7075 is a zinc-alloyed aluminum known for its exceptional strength, comparable to many steels while weighing roughly one-third as much. It is the strongest commonly available aluminum alloy, making it the material of choice where the ultimate strength-to-weight ratio is required.

The T651 temper provides stress-relieved plate with minimal warping during machining. The stress-relief process after solution heat treatment and aging ensures dimensional stability — a critical factor when machining large structural components or precision mold cavities.

7075 is not recommended for welding due to its zinc content and susceptibility to stress corrosion cracking in the weld zone. Joining is typically accomplished through mechanical fastening, adhesive bonding, or friction stir welding for specialized applications.

Widely used in aerospace, defense, and high-stress applications, 7075-T651 plate is produced to AMS 4045 and ASTM B209 standards. All material ships with full mill test certificates (EN 10204 3.1) and ultrasonic inspection reports for thickness above 25 mm.

Chemical Composition of 7075 Aluminum

Nominal chemical composition per ASTM B209 / AMS 4045. All values in weight percent (%).

ElementSiFeCuMnMgCrZnTiAl
Content (%)≤ 0.40≤ 0.501.2 – 2.0≤ 0.302.1 – 2.90.18 – 0.285.1 – 6.1≤ 0.20Balance

Mechanical Properties by Temper

Key mechanical properties for 7075 aluminum plate across common temper conditions.

TemperTensile Strength (MPa)Yield Strength (MPa)Elongation (%)Hardness (HB)
T657250311150
T65157250311150
T735150343411
O (Annealed)22810317

Available Specifications

Full dimensional range and international standard compliance for 7075-T651 aluminum plate.

Plate Dimensions

Thickness6 – 150 mm
WidthUp to 2500 mm
LengthUp to 6000 mm
FlatnessPer AMS 2242 (precision ground on request)
SurfaceMill finish, precision ground
PackagingProtective film, wooden crates, seaworthy

Standards Compliance

AMS 40457075-T651 Aluminum Plate
AMS 40787075-T7351 Aluminum Plate
ASTM B209Standard Specification for Aluminum Plate

Aerospace & Defense Applications

7075-T651 plate is the backbone of modern aerospace structural design, meeting the most demanding AMS specifications.

In the aerospace industry, 7075-T651 aluminum plate serves as the primary structural material for components that must withstand extreme loads while maintaining the lowest possible weight. Its strength-to-weight ratio is unmatched among commonly available aluminum alloys, making it the standard choice for aircraft structural components.

All our 7075-T651 plate is produced to AMS 4045 specification with full material traceability from ingot to finished plate. Ultrasonic inspection per AMS 2154 is standard on plate thicker than 25 mm, ensuring internal soundness for safety-critical applications.

Aircraft Wing Skins & Spars

Upper wing skins, spar caps, and structural stiffeners where the combination of high compressive strength and fatigue resistance is critical for airframe longevity.

Fuselage Frames & Bulkheads

Machined fuselage frames, pressure bulkheads, and floor beams that form the primary load-bearing skeleton of commercial and military aircraft.

Landing Gear Components

Forged and machined landing gear brackets, torque links, and support structures where 7075 provides the necessary strength for repeated high-impact loading.

Missile & Defense Hardware

Missile body sections, launch rail components, radar housings, and military vehicle armor plates requiring MIL-spec material with full lot traceability.

Applications for 7075-T651 Aluminum Plate

From aircraft structures to high-performance sports equipment, 7075 serves the most demanding applications.

Aerospace aluminum plate
7075 plate for high-strength parts
7075 aircraft aluminum sheet
Aircraft-grade aluminum sheet and plate
7075 aluminum plate stock
Precision plate stock for machining

Aircraft Structures

Wing skins, fuselage frames, bulkheads, spars, and structural fittings for commercial and military aircraft.

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Defense & Military

Missile components, military vehicle armor, radar housings, and MIL-spec hardware for defense applications.

Mold & Tooling

Injection mold cavities, blow mold tooling, and precision jig plates where hardness and dimensional stability are required.

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High-Performance Sports

Bicycle frames, climbing gear, ski bindings, and competition-grade sporting equipment demanding maximum strength at minimum weight.

Frequently Asked Questions

Answers to the most common questions about 7075-T651 aluminum plate.

Welding 7075 is generally not recommended. The high zinc content makes it susceptible to hot cracking and stress corrosion cracking in the weld zone. Conventional TIG/MIG welding severely reduces strength in the heat-affected zone. For joining, use mechanical fasteners (bolts, rivets), adhesive bonding, or friction stir welding (FSW) for specialized applications. If welding is absolutely necessary, consult our engineers for recommended procedures and filler alloys.
7075-T651 has higher static strength (572 MPa vs 470 MPa tensile) and hardness, making it better for structural members under compressive loads and mold tooling. 2024-T351 has superior fatigue resistance and damage tolerance, making it preferred for fuselage skins and structures subject to cyclic loading. Both are aerospace-grade alloys with poor weldability. Choose 7075 for maximum strength; choose 2024 for fatigue-critical applications.
T651 is the standard peak-aged temper providing maximum strength (572 MPa tensile). T7351 is an overaged temper that trades approximately 12% strength (503 MPa tensile) for significantly improved resistance to stress corrosion cracking (SCC) and exfoliation corrosion. Use T651 for maximum strength in non-corrosive environments. Use T7351 when the plate will be exposed to corrosive environments or when SCC resistance is a design requirement, such as thick-section aerospace components.
7075 has fair to poor corrosion resistance compared to 5xxx and 6xxx series alloys. It is susceptible to stress corrosion cracking (SCC), especially in the short transverse grain direction. Surface protection is recommended for most applications: anodizing (Type II or Type III), chromate conversion coating, or primer/paint systems. For improved corrosion resistance, consider alclad 7075 (clad with a thin layer of pure aluminum) or the T7351 overaged temper. 7075 should never be used unprotected in marine or high-humidity environments.
7075-T651 has excellent machinability — it is one of the best aluminum alloys for CNC machining. The high zinc and copper content produces clean, well-defined chips that break easily. Recommended cutting speeds are 200–500 m/min with carbide tooling. The T651 stress-relieved temper minimizes distortion during heavy material removal, which is why it is preferred for machined aerospace components. Compared to 6061-T6, 7075 machines slightly cleaner with better chip control, but cutting forces are higher due to the greater hardness.