Clad Aluminum Sheet for Aerospace Panels

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.

Import Duty Rates by Country of Origin

Origin CountryMFN RateCh.99 SurchargesTotal Effective Rate
🇨🇳China2.7%+35.0%37.7%
🇲🇽Mexico2.7%+10.0%12.7%
🇨🇦Canada2.7%+10.0%12.7%
🇩🇪Germany2.7%+10.0%12.7%
🇯🇵Japan2.7%+10.0%12.7%

Alternative Classifications

This product could be classified differently depending on its characteristics or intended use.

7606.12.30Higher: 38% vs 37.7%

If made of aluminum alloys instead of pure aluminum

Aluminum alloys, where Al does not meet 99% purity or other elements exceed limits, shift to alloyed subheading 7606.12.

7606.11.60.00Same rate: 37.7%

If not clad (unclad surface)

Unclad plates/sheets of non-alloyed aluminum fall under 7606.11, as cladding defines the specific subheading.

7610.10.00Higher: 63.2% vs 37.7%

If shaped into doors, covers, or plates with specific profiles

Further worked into shaped aluminum structures for vehicles or buildings moves to Chapter 76 heading 7610 for other aluminum articles.

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Import Tips & Compliance

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

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