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Aluminum alloy sheet metal
for aerospace applications

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Characteristics

Shape

sheet metal

Other characteristics

for aerospace applications

Thickness

Max.: 4 mm
(0.157 in)

0.55 mm, 3.5 mm
(0.022 in, 0.138 in)

Min.: 0.3 mm
(0.012 in)

Width

Max.: 2,600 mm
(102.36 in)

Min.: 1,000 mm
(39.37 in)

Mechanical resistance

Max.: 570,000,000 Pa
(82,671.5 psi)

550,000,000 Pa
(79,770.8 psi)

Min.: 480,000,000 Pa
(69,618.1 psi)

Elasticity

Max.: 500,000,000 Pa
(72,518.9 psi)

480,000,000 Pa
(69,618.1 psi)

Min.: 400,000,000 Pa
(58,015.1 psi)

Description

7A09 T6 Aluminum Alloy Sheet for Aerospace Alloy: 7A09 Temper:T6 thickness: 0.55mm-4.0mm width: 1000mm-2600mm surface: mill finish or at request standard: GB/T3880 、EN485、ASTM B209 Product Description The main alloy element of 7A09 aluminum alloy is zinc, with high strength, good mechanical properties and anode reaction, good plasticity after solution treatment, good heat treatment strengthening effect, good strength below 150 degrees, and particularly good low temperature strength, welding Poor performance, with stress corrosion cracking tendency. 7A09 aluminum sheets are mainly used to manufacture aircraft structures and other high-stress structural parts that require high strength and strong corrosion resistance, such as upper and lower wing wall panels and beams. SPECIFICATION 7A09 T6 aluminum alloy plate: Regular thickness range: 0.3-4mm Regular width range: 1000-2600mm The following table shows the chemical composition of aluminium / aluminum 7A09 alloy. * Remarks: Specific requirement of alloy, temper or specification can be discussed at your request.