7075-T6 Aluminum Alloy Round Bar
A high-strength heat-treatable 7075-T6 aluminum alloy bar with excellent fatigue strength, commonly used in aerospace structural components. It qualifies under HTS 7604.29.50.20 as a bar made from aluminum alloys meeting statistical note 6 criteria for high-strength heat-treatable properties. The T6 temper indicates solution heat-treated and artificially aged for maximum strength.
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Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If not heat-treatable or lower strength
Standard aluminum alloy bars without high-strength heat-treatable properties fall under the general 'other' subheading.
If machined into finished profiles or parts
Machined or further processed bars become 'other articles of aluminum' rather than raw bars/rods.
If hollow and rectangular cross-section
Hollow bars or rods with rectangular profiles are classified separately from solid round bars.
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Import Tips & Compliance
• Verify alloy composition meets statistical note 6 for high-strength heat-treatable alloys with certificates from mill
• Provide detailed temper designation (e.g
• T6) and mechanical properties in documentation to avoid reclassification
• Ensure bars exceed 6mm cross-section to distinguish from wire under chapter notes
Related Products under HTS 7604.29.50.20
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2024-T351 aluminum alloy rod in flat rectangular form, heat-treatable with high strength-to-weight ratio for aircraft fittings. Classified under HTS 7604.29.50.20 due to its high-strength heat-treatable alloy composition as per statistical note 6. The T351 temper provides stress relief after solution heat treatment.
7050-T7451 Aluminum Alloy Bar Stock
7050-T7451 aluminum alloy bar stock optimized for fracture toughness in aerospace forgings. This high-strength heat-treatable alloy per statistical note 6 is classified in HTS 7604.29.50.20. The T7451 temper balances strength with damage tolerance.
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T6 Temper 2014 Aluminum Rod
2014-T6 aluminum rod offering high strength for complex aircraft forgings and structural parts. This heat-treatable alloy qualifies for HTS 7604.29.50.20 under statistical note 6 specifications. Excellent machinability in T6 condition.