7475-T7351 Aluminum Alloy Rod
Premium 7475 aluminum rod in T7351 temper, round cross section, high-strength heat-treatable alloy under statistical note 6 for upper wing skins. Fits HTS 7604.29.30.30 as a bar/rod of qualifying aluminum alloy.
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Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If other statistical note 6 alloys not round-specific
This subheading isolates round cross section high-strength variants.
If drawn into wire <6mm
Wire products distinguished by dimension per subheading note.
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Import Tips & Compliance
• Include fracture toughness data if required for aerospace certification
• Prevent oxidation during shipping with proper packaging to maintain properties
• Declare value per kg accurately; high-value alloys attract scrutiny
Related Products under HTS 7604.29.30.30
7075-T6 Aluminum Round Rod
A high-strength heat-treatable aluminum alloy rod with a round cross section, made from 7075 alloy per statistical note 6, commonly used in aerospace structural components. It qualifies under HTS 7604.29.30.30 due to its specific alloy composition, round cross section, and heat-treatable properties exceeding standard aluminum alloy thresholds. Diameters typically range from 0.5 to 4 inches for precision applications.
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Round cross-section bar from 2024 high-strength heat-treatable aluminum alloy, heat-treated to T3 temper for aircraft skin and structural use as defined in statistical note 6. This product fits HTS 7604.29.30.30 precisely due to its alloy type, round shape, and enhanced mechanical properties from heat treatment. Ideal for high-stress aviation components.
7050-T7451 Aluminum Rod
High-strength 7050 aluminum alloy rod in T7451 temper with round cross section, designed for aerospace forgings and listed in statistical note 6. Classified under HTS 7604.29.30.30 for its heat-treatable properties, aluminum alloy composition, and bar/rod form. Used in fuselage frames and wing spars.
7178-T651 Aluminum Round Bar
7178 alloy round bar heat-treated to T651 condition, a high-strength option for aircraft per statistical note 6, with round cross section qualifying for HTS 7604.29.30.30. Its heat-treatable nature and alloy composition make it distinct from standard alloys.