Nickel Alloy Compressor Stator Vane from China
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.
Duty Rate — China → United States
35%
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
9903.88.0125%Except as provided in headings 9903.88.05, 9903.88.06, 9903.88.07, 9903.88.08, 9903.88.10, 9903.88.11, 9903.88.14, 9903.88.19, 9903.88.50, 9903.88.52, 9903.88.58, 9903.88.60, 9903.88.62, 9903.88.66, 9903.88.67, 9903.88.68, or 9903.88.69, articles the product of China, as provided for in U.S. note 20(a) to this subchapter and as provided for in the subheadings enumerated in U.S. note 20(b) [to this subchapter]
Import Tips
• 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