Composite Helicopter Main Rotor Blade from Canada
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 — Canada → United States
100%
Rate breakdown
9903.08.21100%Except as provided in headings 9903.08.23–9903.08.26, unmanned aircraft, their parts and components, as provided for in subdivisions (c)(1)–(3) of U.S. note 43 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
• 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