7050-T7451 Aluminum Rod from Japan
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.
Duty Rate — Japan → United States
52.6%
Rate breakdown
9903.82.0250%Except as provided for in headings 9903.82.14, 9903.85.67 and 9903.85.68, articles of aluminum, of steel or of copper and derivative aluminum or steel articles, as provided for in subdivisions (c)(i)–(v) of U.S. note 16 to this subchapter
9903.05.900%Articles already subject to Section 232 (steel/aluminum/copper + derivatives, autos + parts, wood, medium/heavy vehicles + parts, semiconductors, patented pharma) — U.S. note 52(f)
Import Tips
• Submit alloy chemistry analysis confirming >1% other elements per subheading note (b) for alloy status
• Document end-use if for defense/aerospace to prepare for ITAR or EAR licensing requirements
• Avoid bundling with fittings, as sets could classify under 7616 as articles