Chemical composition Element Limit in wt percent Silicon Si ≤0.40 Iron Fe ≤0.50 Copper Cu 1.20–2.00 Manganese Mn ≤0.30 Magnesium Mg 2.10–2.90 Chromium Cr 0.18–0.28 Zinc Zn 5.10–6.10 Titanium Ti ≤0.20 Other elements each ≤0.05 Other elements total ≤0.15 Aluminum Al Balance

Mechanical properties by temper Temper Condition or thickness Rm MPa Rp0.2 MPa Elongation % Basis O Annealed 228 103 16 Typical flat product [7] T6 Artificial aging 572 503 11 Typical flat product [7] T651 6.35–101.60 mm plate 462–538 372–462 3–9 Minima span LT [13] T7351 6.35–101.60 mm plate 421–476 331–393 6–7 Minima span LT [13]

Application fields Machined aircraft structural components, fittings and reinforcement plates. High-load fixtures, tooling and precision mechanical components. Defense and ordnance components requiring high specific strength. Performance sporting and transport components produced by machining.

Chemical composition Element Limit in wt percent Silicon Si ≤0.40 Iron Fe ≤0.50 Copper Cu 1.20–2.00 Manganese Mn ≤0.30 Magnesium Mg 2.10–2.90 Chromium Cr 0.18–0.28 Zinc Zn 5.10–6.10 Titanium Ti ≤0.20 Other elements each ≤0.05 Other elements total ≤0.15 Aluminum Al Balance

Mechanical properties by temper Temper Condition or thickness Rm MPa Rp0.2 MPa Elongation % Basis O Annealed 228 103 16 Typical flat product [7] T6 Artificial aging 572 503 11 Typical flat product [7] T651 6.35–101.60 mm plate 462–538 372–462 3–9 Minima span LT [13] T7351 6.35–101.60 mm plate 421–476 331–393 6–7 Minima span LT [13]

Application fields Machined aircraft structural components, fittings and reinforcement plates. High-load fixtures, tooling and precision mechanical components. Defense and ordnance components requiring high specific strength. Performance sporting and transport components produced by machining.

7075 Aluminum Plate/Sheet

Grade: 7075

Coil: 0.3mm-3.0mm

Sheet: 0.3mm-300mm

Width: 50mm-2000mm

Standard: ASTM, AMS, BS etc.

7075 is a high-strength aluminum zinc magnesium copper alloy used for demanding aerospace and mechanical components. T6 and T651 prioritize strength, while T73 and T7351 sacrifice some strength to improve stress corrosion resistance. The alloy machines well in hardened conditions but has limited formability and is generally unsuitable for conventional fusion welded structural assemblies. Protective finishing and careful control of grain direction are important for critical applications. Plate is widely used for machined load carrying parts and tooling.

Chemical composition

Element	Limit in wt percent
Silicon Si	≤0.40
Iron Fe	≤0.50
Copper Cu	1.20–2.00
Manganese Mn	≤0.30
Magnesium Mg	2.10–2.90
Chromium Cr	0.18–0.28
Zinc Zn	5.10–6.10
Titanium Ti	≤0.20
Other elements each	≤0.05
Other elements total	≤0.15
Aluminum Al	Balance

Mechanical properties by temper

Temper	Condition or thickness	Rm MPa	Rp0.2 MPa	Elongation %	Basis
O	Annealed	228	103	16	Typical flat product [7]
T6	Artificial aging	572	503	11	Typical flat product [7]
T651	6.35–101.60 mm plate	462–538	372–462	3–9	Minima span LT [13]
T7351	6.35–101.60 mm plate	421–476	331–393	6–7	Minima span LT [13]

Application fields

Machined aircraft structural components, fittings and reinforcement plates.
High-load fixtures, tooling and precision mechanical components.
Defense and ordnance components requiring high specific strength.
Performance sporting and transport components produced by machining.

Introduction

Specification

Chemical composition

Element	Limit in wt percent
Silicon Si	≤0.40
Iron Fe	≤0.50
Copper Cu	1.20–2.00
Manganese Mn	≤0.30
Magnesium Mg	2.10–2.90
Chromium Cr	0.18–0.28
Zinc Zn	5.10–6.10
Titanium Ti	≤0.20
Other elements each	≤0.05
Other elements total	≤0.15
Aluminum Al	Balance

Mechanical

Mechanical properties by temper

Temper	Condition or thickness	Rm MPa	Rp0.2 MPa	Elongation %	Basis
O	Annealed	228	103	16	Typical flat product [7]
T6	Artificial aging	572	503	11	Typical flat product [7]
T651	6.35–101.60 mm plate	462–538	372–462	3–9	Minima span LT [13]
T7351	6.35–101.60 mm plate	421–476	331–393	6–7	Minima span LT [13]