Nozzle Guide Vane for LEAP-1A Engine from China
Single-crystal superalloy nozzle guide vane (NGV) for the hot-section transition in CFM LEAP-1A turbofan powering Airbus A320neo. Features advanced cooling passages for turbine inlet temperatures. HTS 8411.99.90.90 as stationary aircraft gas turbine hardware.
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
• Include thermal barrier coating specifications and EASA Form 1 airworthiness tag
• Declare as 'OEM replacement part' with serial number traceability