Composite Helicopter Main Rotor Blade from China
A lightweight main rotor blade constructed from carbon fiber composites for helicopters under heading 8802. It functions as a critical aerodynamic component to generate lift during flight. Classified under 8807.10.00.60 as a part of rotor for aircraft of heading 8802.
Duty Rate — China → United States
35%
Rate breakdown
9903.03.0110%Except for products described in headings 9903.03.02–9903.03.11, articles the product of any country, as provided for in subdivision (aa) of U.S. note 2 to this subchapter
9903.88.0125%Except as provided in headings 9903.88.05, 9903.88.06, 9903.88.07, 9903.88.08, 9903.88.10, 9903.88.11, 9903.88.14, 9903.88.19, 9903.88.50, 9903.88.52, 9903.88.58, 9903.88.60, 9903.88.62, 9903.88.66, 9903.88.67, 9903.88.68, or 9903.88.69, articles the product of China, as provided for in U.S. note 20(a) to this subchapter and as provided for in the subheadings enumerated in U.S. note 20(b) [to this subchapter]
Import Tips
• Obtain FAA or EASA certification documentation to verify airworthiness compliance during customs clearance
• Declare exact material composition (e.g
• carbon fiber percentage) to avoid reclassification under general machinery parts
• Include manufacturer specs confirming unladen weight compatibility for helicopters under 8802