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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%Section 301 (forced labor) — Japan (col1 rate < 12.5 percent): MFN < 12.5% → total duty capped at 12.5%

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