Clad Aluminum Sheet for Aerospace Panels from Germany
A high-purity, non-alloyed aluminum sheet clad with a thin protective layer, measuring 5 mm thick, used in aircraft fuselage panels. It falls under HTS 7606.91.60.95 due to its clad construction, aluminum content over 99%, thickness between 0.2 mm and 6.3 mm, and plate/sheet form exceeding 0.2 mm.
Duty Rate — Germany → United States
52.7%
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 of aluminum, of steel or of copper or derivative aluminum or steel articles; passenger vehicles (sedans, sport utility vehicles, crossover utility vehicles, minivans and cargo vans) and light trucks; parts of passenger vehicles (sedans, sport utility vehicles, crossover utility vehicles, minivans and cargo vans) and light trucks; medium- and heavy-duty vehicles; parts of medium- and heavy-duty vehicles; wood products; patented pharmaceutical articles; and semiconductor articles, as provided in subdivision (f) of U.S. note 52 to this subchapter
Import Tips
• Verify aluminum purity exceeds 99% with Fe+Si ≤0.1% via mill test certificates to confirm non-alloyed status
• Provide cladding specifications and thickness measurements in entry documentation to avoid misclassification as unclad
• Ensure proper marking of country of melt and pour per Commerce Control List requirements for aluminum articles