Turbojet Turbine Nozzle Guide Vane from Mexico
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 — Mexico → United States
10%
Rate breakdown
9903.05.5510%Except for products described in headings 9903.05.85–9903.05.92 and 9903.05.94, articles the product of Mexico, as provided for in U.S. note 52 to this subchapter
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