Aircraft Gas Turbine Combustion Liner from Japan
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 — Japan → United States
12.5%
Rate breakdown
9903.05.4912.5%Except for products described in headings 9903.05.85–9903.05.92, articles the product of Japan, with an ad valorem (or ad valorem equivalent) rate of duty under column 1 less than 12.5 percent, as provided for in U.S. note 52 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