Aircraft Turbine Engine Compressor Blade from Canada
A precision-machined titanium compressor blade designed exclusively for use in aircraft gas turbine engines under heading 8407. It operates in the high-pressure compressor section to accelerate airflow. Classified under 8409.10.0080 as a part solely for aircraft engines, distinct from general aviation propellers.
Duty Rate — Canada → United States
10%
Rate breakdown
9903.05.2910%Except for products described in headings 9903.05.85–9903.05.93, articles the product of Canada, as provided for in U.S. note 52 to this subchapter
Import Tips
• Obtain FAA or EASA certification documents proving the part's aircraft engine compatibility to avoid reclassification
• Declare exact material composition (e.g
• titanium alloy) as it affects duty rates and ITAR export controls
• Avoid common pitfall of insufficient Bills of Materials (BOM) linking the part to specific 8407 engine models