Turbojet Turbine Nozzle Guide Vane from China
Stator vanes that direct high-temperature exhaust gases onto turbine blades in turbojet engines, made from heat-resistant nickel alloys. Classified under HTS 8411.91.90 as an 'other' part of turbojets, distinct from compressor blades or engine casings. Critical for optimizing engine efficiency and thrust.
Duty Rate — China → United States
37.5%
Rate breakdown
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]
9903.05.3112.5%Section 301 (forced labor) — additional 12.5% ad valorem on products of China
Import Tips
• Include heat treatment and alloy composition certificates to meet import material traceability requirements
• Label clearly as aircraft engine parts to prevent reclassification as industrial components
• Watch for anti-dumping duties on certain alloy imports from specific countries