HS code / TARIC details
8411990030 - 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
Definition & language versions
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
Tip: confirm material, use and finished-product form first, then compare hierarchy and declarable candidates below.
ZH
涡轮增压器涡轮壳体,带安装涡轮叶轮的孔,孔径28-181毫米
DE
Turbinengehäuse von Abgasturboladern, mit einer Aussparung zur Aufnahme eines Turbinenrades, die einen Durchmesser von 28mm oder mehr, jedoch nicht mehr als 181mm, aufweist
EN
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
Classification hints
This code appears to be a directly declarable leaf candidate and can be used for the next customs-filing step.
Please check validity dates and duty effective dates, as the applicable rule may depend on the filing date.
Codes
TARIC
84119900 30
CN (8 digits)
84119900
HS (6 digits)
841199
Updated at
Mon Aug 31
Duty
Duty rate (import)
0.000%
Effective from
Thu Jan 01
Legal base
Regulation 2605/25
Validity & quantity
Start date
Mon Jan 01
End date
-
Supplementary unit
Not required
Code hierarchy
TARIC
Trade measures and restrictions
This block shows a filing-oriented summary first, then imported TARIC measures including scope, add. codes, order numbers, duty expressions and legal bases.
Imported measures: 1Country-scoped: 0With add. code/order: 0
Measure
Current value
Notes / validity
Reference import duty
0.000%
Effective from Thu Jan 01
Legal base
Regulation 2605/25
-
Supplementary unit
Not required
Validity: Mon Jan 01 - -
Imported TARIC measures
Measure
Scope
Duty / codes
Validity
Legal base
Supplementary unit import
110
All origins (erga omnes)
NAR
Sat Jan 01 - -
Regulation 2278/21
Siblings
8411990010
Of gas turbines, for use in civil aircraft
8411990020
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
8411990045
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
8411990099
Other
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TARIC change hints
After a monthly TARIC update, this block shows a hint about text changes versus the previous snapshot.
Source: internal TARIC diff (hint only)
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Current
Turbinengehäuse von Abgasturboladern, mit einer Aussparung zur Aufnahme eines Turbinenrades, die einen Durchmesser von 2
Type: newSource lang: EN+DE
Next actions
If this code looks suitable for your product, continue with shipment creation or customs-entry forms.