HS code / TARIC details
8411990010 - Of gas turbines, for use in civil aircraft
Definition & language versions
Of gas turbines, for use in civil aircraft
Tip: confirm material, use and finished-product form first, then compare hierarchy and declarable candidates below.
ZH
燃气轮机零件,民用飞机用
DE
von Gasturbinen für zivile Luftfahrzeuge
EN
Of gas turbines, for use in civil aircraft
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 10
CN (8 digits)
84119900
HS (6 digits)
841199
Updated at
Mon Aug 31
Duty
Duty rate (import)
0.000%
Effective from
Mon Jan 01
Legal base
Regulation 1549/06
Validity & quantity
Start date
Sun Jan 01
End date
-
Supplementary unit
Not required
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.
Measure
Current value
Notes / validity
Reference import duty
0.000%
Effective from Mon Jan 01
Legal base
Regulation 1549/06
-
Supplementary unit
Not required
Validity: Sun Jan 01 - -
Imported TARIC measures
No detailed TARIC measures are available for this code in the current import yet. Use the summary above and verify against the official TARIC page.
Siblings
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
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
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
This page provides public lookup and helper information only and is not customs/tax/legal advice. Official TARIC/EZT sources prevail.
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)
Previous
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Current
von Gasturbinen für zivile Luftfahrzeuge
Type: newSource lang: EN+DE
Next actions
If this code looks suitable for your product, continue with shipment creation or customs-entry forms.