Turbine Blade for CFM56 Aircraft Engine from China
A high-precision nickel-based superalloy turbine blade designed specifically for the high-pressure turbine stage of the CFM56 turbofan engine used on Boeing 737 and Airbus A320 aircraft. It falls under HTS 8411.99.90.90 as it is an essential rotating part dedicated to aircraft gas turbine operation, engineered for extreme temperatures and stresses.
Duty Rate — China → United States
37.4%
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
• Obtain FAA or EASA certification documentation proving aircraft-specific use to avoid reclassification
• Provide detailed engineering specs and OEM part numbers; common pitfall is insufficient traceability leading to delays
• Declare exact material composition (e.g
• Inconel alloys) for accurate duty assessment and ITAR compliance