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Aircraft Gas Turbine Combustion Liner

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.

Import Duty Rates by Country of Origin

Origin CountryMFN RateCh.99 SurchargesTotal Effective Rate
🇨🇳ChinaFree+35.0%35%
🇲🇽MexicoFree+10.0%10%
🇨🇦CanadaFree+10.0%10%
🇩🇪GermanyFree+10.0%10%
🇯🇵JapanFree+10.0%10%

More Specific Codes

This product may fall under a more specific subheading:

Alternative Classifications

This product could be classified differently depending on its characteristics or intended use.

8411.99.90Higher: 37.4% vs 35%

If designed for stationary marine gas turbines

Gas turbine parts in 8411 for non-aero use; aircraft principal use keeps it in 8409.

6903.20.00Same rate: 35%

If ceramic liners without metal integration

Refractory ceramics in 6903 for high-temp non-mechanical parts.

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Import Tips & Compliance

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