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%Section 301 (forced labor) — Japan (col1 rate < 12.5 percent): MFN < 12.5% → total duty capped at 12.5%
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