Aircraft Gas Turbine Combustion Liner from Canada
Heat-resistant combustion chamber liner for aircraft gas turbine engines, preventing fuel-air mixture leaks. HTS 8409.10.00 applies as it's principally for aircraft engines of 8407/8408.
Duty Rate — Canada → United States
10%
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
Import Tips
• Provide thermal imaging test results proving aircraft-grade heat tolerance over 1500°C
• Comply with REACH for nickel alloys; declare hazardous material handling if applicable
• Avoid reclassification as general furnace parts (8417); submit engine integration diagrams