Turbojet Inlet Guide Vane Ring from Mexico
Circumferential ring of adjustable inlet guide vanes controlling airflow into turbojet compressors. Falls under HTS 8411.91.90 as other turbojet parts, integral stator assembly. Optimizes engine performance from startup to cruise.
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
• Airflow coefficient documentation proves aerodynamic specificity
• Specify variable pitch mechanism details
• Avoid 'fan stator' declaration used for turbofans