CN 8411
Turbojets, turbopropellers and other gas turbines
| Code | Description | Unit | Third-country duty | Source |
|---|---|---|---|---|
| Turbojets | ||||
| 8411 11 | Of a thrust not exceeding 25 kN | TARIC | ||
| 8411 11 00 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 11 00 20 | Intended to be fitted in aircraft imported duty free or built within the Community | p/st | 0% (end-use) | TARIC |
| 8411 11 00 90 | Other | p/st | 3.2% | TARIC |
| 8411 12 | Of a thrust exceeding 25 kN | TARIC | ||
| 8411 12 10 | Of a thrust exceeding 25 kN but not exceeding 44 kN | TARIC | ||
| 8411 12 10 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 12 10 20 | Intended to be fitted in aircraft imported duty free or built within the Community | p/st | 0% (end-use) | TARIC |
| 8411 12 10 90 | Other | p/st | 2.7% | TARIC |
| 8411 12 30 | Of a thrust exceeding 44 kN but not exceeding 132 kN | TARIC | ||
| 8411 12 30 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 12 30 20 | Intended to be fitted in aircraft imported duty free or built within the Community | p/st | 0% (end-use) | TARIC |
| 8411 12 30 90 | Other | p/st | 2.7% | TARIC |
| 8411 12 80 | Of a thrust exceeding 132 kN | TARIC | ||
| 8411 12 80 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 12 80 20 | Intended to be fitted in aircraft imported duty free or built within the Community | p/st | 0% (end-use) | TARIC |
| 8411 12 80 90 | Other | p/st | 2.7% | TARIC |
| Turbopropellers | ||||
| 8411 21 | Of a power not exceeding 1 100 kW | TARIC | ||
| 8411 21 00 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 21 00 20 | Intended to be fitted in aircraft imported duty free or built within the Community | p/st | 0% (end-use) | TARIC |
| 8411 21 00 90 | Other | p/st | 3.6% | TARIC |
| 8411 22 | Of a power exceeding 1 100 kW | TARIC | ||
| 8411 22 20 | Of a power exceeding 1 100 kW but not exceeding 3 730 kW | TARIC | ||
| 8411 22 20 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 22 20 20 | Intended to be fitted in aircraft imported duty free or built within the Community | p/st | 0% (end-use) | TARIC |
| 8411 22 20 90 | Other | p/st | 2.7% | TARIC |
| 8411 22 80 | Of a power exceeding 3 730 kW | TARIC | ||
| 8411 22 80 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 22 80 20 | Intended to be fitted in aircraft imported duty free or built within the Community | p/st | 0% (end-use) | TARIC |
| 8411 22 80 90 | Other | p/st | 2.7% | TARIC |
| Other gas turbines | ||||
| 8411 81 | Of a power not exceeding 5 000 kW | TARIC | ||
| 8411 81 00 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 81 00 90 | Other | p/st | 4.1% | TARIC |
| 8411 82 | Of a power exceeding 5 000 kW | TARIC | ||
| 8411 82 20 | Of a power exceeding 5 000 kW but not exceeding 20 000 kW | TARIC | ||
| 8411 82 20 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 82 20 90 | Other | p/st | 4.1% | TARIC |
| 8411 82 60 | Of a power exceeding 20 000 kW but not exceeding 50 000 kW | TARIC | ||
| 8411 82 60 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 82 60 90 | Other | p/st | 4.1% | TARIC |
| 8411 82 80 | Of a power exceeding 50 000 kW | TARIC | ||
| 8411 82 80 10 | For use in civil aircraft | p/st | 0% (end-use) | TARIC |
| 8411 82 80 90 | Other | p/st | 4.1% | TARIC |
| Parts | ||||
| 8411 91 | Of turbojets or turbopropellers | TARIC | ||
| 8411 91 00 10 | For use in civil aircraft | 0% (end-use) | TARIC | |
| 8411 91 00 20 | Intended to be fitted in aircraft imported duty free or built within the Community | 0% (end-use) | TARIC | |
| 8411 91 00 90 | Other | 2.7% | TARIC | |
| 8411 99 | Other | TARIC | ||
| 8411 99 00 10 | Of gas turbines, for use in civil aircraft | 0% (end-use) | TARIC | |
| Other | ||||
| 8411 99 00 20 | Wheel-shaped gas turbine component with blades, of a kind used in turbochargers: - of a precision-cast nickel based alloy complying with standard DIN G- NiCr13Al6MoNb or DIN G- NiCr13Al16MoNb or DIN G- NiCo10W10Cr9AlTi or DIN G- NiCr12Al6MoNb or AMS AISI:686, - with a heat-resistance of not more than 1 100 °C, - with a diameter of 28 mm or more, but not more than 180 mm, - with a height of 20 mm or more, but not more than 150 mm | p/st | 4.1% | TARIC |
| 8411 99 00 30 | Turbine housing of turbochargers, with a hole to insert a turbine wheel, whereby the hole has a diameter of 28mm or more, but not more than 181mm | p/st | 4.1% | TARIC |
| 8411 99 00 45 | Turbine ring segments, guide and rotor blades as parts of a stationary gas turbine for power generation or as a mechanical drive - made of nickel-based superalloys, - for an operating temperature of more than 600 K but not more than 1600 K, - with a length of not more than 500 mm, - with a width of not more than 900 mm, - with a height of not more than 1300 mm | 4.1% | TARIC | |
| 8411 99 00 99 | Other | 4.1% | TARIC | |
The table scrolls sideways.
Source: European Commission (DG TAXUD), TARIC and Combined Nomenclature data as extracted on 1 October 2026. Heading 8411 in the TARIC consultation
Only the third-country duty is shown. Not shown: tariff preferences, quotas, suspensions, anti-dumping and other additional duties, import controls and the legal notes. The TARIC consultation lists the measures of each code.
This page is general information, not legal advice and not a classification decision. Tariff texts and rates change: check the publisher's current schedule, and ask the customs authority for a binding ruling where the answer matters.