SAE Aerospace Material Specifications

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Standard [CURRENT] 2022-11-02

SAE AMS 4367A:2022-11-02

Aluminum Alloy, Extruded Profiles, 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T74511), Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 4.500 inches (1.02 to 114.30 mm), inclusive, in thickness produced with maximum cross ...

80.40 EUR VAT included

75.14 EUR VAT excluded
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Standard [CURRENT] 2023-03-08

SAE AMS 4368A:2023-03-08

Aluminum Alloy, Discontinuously Reinforced Hot Isostatically Pressed Shapes 6061B/SiC/40p (3 Î¼m) (T1P)

This specification covers discontinuously reinforced aluminum alloy (DRA) metal matrix composites (MMC) made by mechanical alloying of 6061B aluminum powder and SiC particulate, which is then ...

80.40 EUR VAT included

75.14 EUR VAT excluded
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Standard [CURRENT] 2024-10-28

SAE AMS 4369A:2024-10-28

Aluminum Alloy, Discontinuously Reinforced Extruded Bar, Rod, Wire and Shapes, (2124A/SiC/25p (0.7 µm) (T1P)

This specification covers a discontinuously reinforced aluminum alloy (DRA) made by mechanical alloying 2124A aluminum powder and silicon carbide particulate (SiC). It is produced in the form of ...

73.50 EUR VAT included

68.69 EUR VAT excluded
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Standard [CURRENT] 2023-12-13

SAE AMS 4371C:2023-12-13

Magnesium Alloy, Plate 4.0Y - 2.25Nd - 0.5Zr (WE43C - T5) Precipitation Heat Treated

This specification covers a magnesium alloy in the form of rolled plate from 0.500 up to 6.0 inches (12.7 to 152.4 mm), inclusive (see 8.5).

80.40 EUR VAT included

75.14 EUR VAT excluded
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Standard [CURRENT] 2022-08-05

SAE AMS 4372B:2022-08-05

Aluminum Alloy, Plate 3.5Cu - 1.0Li - 0.40Mg - 0.35Mn - 0.45Ag - 0.12Zr (2050-T34) Solution Heat Treated and Stress Relieved

This specification covers an aluminum-lithium alloy in the form of plate 0.500 to 6.500 inches (12.70 to 165.00 mm) in nominal thickness (see 8.6).

80.40 EUR VAT included

75.14 EUR VAT excluded
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Standard [CURRENT] 2024-09-09

SAE AMS 4373A:2024-09-09

Aluminum Alloy, Rolled, Drawn or Cold Finished Bar, Rod, and Wire 4.0Cu - 0.70Mn - 0.60Mg - 0.50Si (2017; -O or when ordered -F)

This specification covers the specific requirements for 2017 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing supplied in the annealed (O temper) condition (see 8.4).

86.30 EUR VAT included

80.65 EUR VAT excluded
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Standard [CURRENT] 2022-11-02

SAE AMS 4374A:2022-11-02

Aluminum Alloy, Extruded Profiles 8.9Zn - 2.2Cu - 2.2Mg - 0.15Zr (7136-T73511) Solution Heat Treated, Stress Relieved by Stretching, Straightened, and Overaged

This specification covers an aluminum alloy in the form of extruded rods, bars, and profiles (shapes) 0.040 to 4.500 inches (1.02 to 114.30 mm), inclusive, in thickness produced with maximum cross ...

80.40 EUR VAT included

75.14 EUR VAT excluded
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Standard [CURRENT] 2024-05-01

SAE AMS 4375N:2024-05-01

Sheet and Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-O) Annealed and Recrystallized

This specification covers a magnesium alloy in the form of sheet and plate from 0.016 to 3.000 inches (0.41 to 76.20 mm), inclusive, in thickness (see 8.5).

73.50 EUR VAT included

68.69 EUR VAT excluded
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Standard [CURRENT] 2018-11-07

SAE AMS 4376H:2018-11-07

Plate, Magnesium Alloy 3.0Al - 1.0Zn - 0.20Mn (AZ31B-H26) Cold Rolled and Partially Annealed

This specification covers a magnesium alloy in the form of plate.

73.50 EUR VAT included

68.69 EUR VAT excluded
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Standard [NEW] 2025-06-17

SAE AMS 4377K:2025-06-17

Magnesium Alloy, Sheet and Plate, 3.0Al - 1.0Zn - 0.20Mn (AZ31B-H24), Cold Rolled, Partially Annealed

This specification covers a magnesium alloy in the form of sheet and plate 0.016 to 3.000 inches (0.41 to 76.20 mm) in nominal thickness (see 8.6).

80.30 EUR VAT included

75.05 EUR VAT excluded
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