Turbojet Combustion Chamber Liner from United States
An inner liner of the annular combustion chamber in turbojet engines, perforated for fuel-air mixing and cooled by airflow. It is made from high-temperature alloys and is classified as a part of a turbojet under tariff item 8411.91.00.
Duty Rate — United States → Canada
0%
Import Tips
• Classify the liner as a part of a turbojet under 8411.91.00, not as a complete combustion chamber
• Provide material certifications and engineering drawings to the CBSA to confirm its specific use
• Be aware that liners with additional features, like igniters, may be classified differently