Turbine Compressor Rotor Assembly from Japan
A precision-engineered rotor assembly used in the compressor section of turbojet engines, consisting of multiple blades mounted on a central disk. It falls under HTS 8411.91.90 as a part specifically designed for turbojets, not covered by more specific subheadings like casings or brackets. This component compresses incoming air to high pressure before combustion.
Duty Rate — Japan → United States
12.5%
Rate breakdown
9903.05.4912.5%Except for products described in headings 9903.05.85–9903.05.92, articles the product of Japan, with an ad valorem (or ad valorem equivalent) rate of duty under column 1 less than 12.5 percent, as provided for in U.S. note 52 to this subchapter
Import Tips
• Verify part certification with FAA or EASA approvals to ensure compliance with aviation safety standards
• Provide detailed engineering drawings and material specs in documentation to avoid misclassification