MACHINERY AND MECHANICAL APPLIANCES > NUCLEAR REACTORS, BOILERS, MACHINERY AND MECHANICAL APPLIANCES; PARTS THEREOF > Turbojets, turbopropellers and other gas turbines
| Code | Description | Duty |
|---|---|---|
| 8411110000 | Turbojets | - |
| 8411110000 | Of a thrust not exceeding 25|kN | - |
| 8411110010D | For use in civil aircraft | - |
| 8411110020D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| 8411110090D | Other | 3.200 % |
+53 sub-codes
| Intended to be fitted in aircraft imported duty free or built within the Community |
| - |
| D | Other | 3.200 % |
| Of a thrust exceeding 25|kN | - |
| Of a thrust exceeding 25|kN but not exceeding 44|kN | - |
| D | For use in civil aircraft | - |
| D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| D | Other | 2.700 % |
| Of a thrust exceeding 44|kN but not exceeding 132|kN | - |
| D | For use in civil aircraft | - |
| D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| D | Other | 2.700 % |
| Of a thrust exceeding 132|kN | - |
| D | For use in civil aircraft | - |
| D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| D | Other | 2.700 % |
| Turbopropellers | - |
| Of a power not exceeding 1|100|kW | - |
| D | For use in civil aircraft | - |
| D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| D | Other | 3.600 % |
| Of a power exceeding 1|100|kW | - |
| Of a power exceeding 1|100|kW but not exceeding 3|730|kW | - |
| D | For use in civil aircraft | - |
| D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| D | Other | 2.700 % |
| Of a power exceeding 3|730|kW | - |
| D | For use in civil aircraft | - |
| D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| D | Other | 2.700 % |
| Other gas turbines | - |
| Of a power not exceeding 5|000|kW | - |
| D | For use in civil aircraft | - |
| D | Other | 4.100 % |
| Of a power exceeding 5|000|kW | - |
| Of a power exceeding 5|000|kW but not exceeding 20|000|kW | - |
| D | For use in civil aircraft | - |
| D | Other | 4.100 % |
| Of a power exceeding 20|000|kW but not exceeding 50|000|kW | - |
| D | For use in civil aircraft | - |
| D | Other | 4.100 % |
| Of a power exceeding 50|000|kW | - |
| D | For use in civil aircraft | - |
| D | Other | 4.100 % |
| Parts | - |
| Of turbojets or turbopropellers | - |
| D | For use in civil aircraft | - |
| D | Intended to be fitted in aircraft imported duty free or built within the Community | - |
| D | Other | 2.700 % |
| Other | - |
| D | Of gas turbines, for use in civil aircraft | - |
| Other | 4.100 % |
| D | 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 | 4.100 % |
| D | 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 | 4.100 % |
| D | 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 | 4.100 % |
| D | Other | 4.100 % |
CTH; or 45% value added rule
CTH; or 45% value added rule