Nickel Alloy Compressor Stator Vane

High-temperature nickel superalloy stator vane for the compressor section of commercial aircraft turbofan engines. Directs airflow efficiently while enduring corrosive environments. Falls under HTS 8411.91.90.85 as an other part of aircraft turbojet/turbopropeller.

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%

Alternative Classifications

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

8411.91.10Same rate: 35%

If specifically a casing or housing component

Aircraft turbine casings have dedicated subheading 8411.91.10 separate from other parts.

7224.90Lower: 10% vs 35%

If imported as raw nickel alloy bar stock for later machining

Semi-finished nickel products classified by material composition in Chapter 72 before fabrication.

Not sure which classification is right?

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Import Tips & Compliance

Provide turbine engine serial number references and blueprints to substantiate aircraft classification

Comply with ITAR/EAR licensing if US-origin technology; declare technical data accurately

Watch for undervaluation penalties - use OEM pricing data for proper dutiable value

Related Products under HTS 8411.91.90.85

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Single-crystal superalloy HPT shroud segment with abradable coating for tip clearance control in aircraft engines. Protects turbine case from blade wear. HTS 8411.91.90.85 for other aircraft turbine parts.

Titanium Turbine Blade for Aircraft Turbojet

Precision-engineered titanium high-pressure turbine blade designed specifically for aircraft turbojet engines. It withstands extreme temperatures and rotational stresses in the turbine section. Classified under HTS 8411.91.90.85 as a part of turbojets used in aircraft.

Combustor Liner Segment for Turbofan Engine

Ceramic matrix composite combustor liner segment for next-generation high-bypass turbofan engines used in widebody aircraft. Provides thermal protection and reduces weight. HTS 8411.91.90.85 classification for aircraft turbine combustor parts.

Aircraft Turbine Bearing Housing

Precision-machined bearing housing assembly for main shaft bearings in high-performance aircraft turboprops. Made from high-strength steel alloy with specialized coatings. Classified as other aircraft turbine parts under 8411.91.90.85.

Turbine Nozzle Guide Vane Ring

Monolithic nozzle guide vane ring assembly for aircraft gas turbine hot section, manufactured via investment casting. Controls hot gas flow to turbine blades. HTS 8411.91.90.85 as other turbojet parts for aircraft.

Aircraft Engine Fuel Nozzle Assembly

Duplex fuel nozzle assembly with integrated swirler for lean-burn combustors in modern aircraft turbofans. Ensures optimal fuel-air mixing for emissions compliance. Classified under 8411.91.90.85 as aircraft turbine part.