Customs tariff code

Customs tariff code 8411.99.00.10: Of gas turbines, for use in civil aircraft

Reference data as at 1 July 2026

Customs tariff code 8411.99.00.10 covers Of gas turbines, for use in civil aircraft. TARIC holds no third-country duty rate of its own for this code; the rate follows from the declarable commodity code beneath it.

8411.99.00.10 is TARIC code in the EU customs tariff, in chapter 84. This page shows the full classification path, the duty rate, the official comparison cases, and the notes that govern this code.

This code is not declarable on its own. A declaration needs one of the subdivisions beneath it.

Customs code
8411.99.00.10
Third-country duty
See subdivision
Declarable
No
Binding rulings
8

Where this code sits in the tariff

  1. 84NUCLEAR REACTORS, BOILERS, MACHINERY AND MECHANICAL APPLIANCES; PARTS THEREOF
  2. 8411Turbojets, turbopropellers and other gas turbines
  3. 8411.99Other
  4. 8411.99.00Teile, andere
  5. 8411.99.00.10Of gas turbines, for use in civil aircraft

From HS code to customs tariff code 8411.99.00.10

HS code8411.996 digits, uniform worldwide
CN code8411.99.008 digits, EU Combined Nomenclature
TARIC code8411.99.00.1010 digits, carries the EU measures

Duty rates and preferences

OriginDuty rateBasis
Faroe Islands0 %Tariff preference
Melilla0 %Tariff preference
Occupied palestinian Territory0 %Tariff preference
Türkiye0 %Customs Union Duty
San Marino0 %Customs Union Duty
Andorra0 %Customs Union Duty
EU-Switzerland agreement: re-imported goods0 %Tariff preference
GSP+ (incentive arrangement for sustainable development and…0 %Tariff preference
GSP-EBA (Special arrangement for the least-developed countries…0 %Tariff preference
Moldova, Republic of0 %Tariff preference
Ecuador0 %Tariff preference
United Kingdom0 %Tariff preference

Rates from the EU TARIC database. Preferential rates require valid proof of origin.

Compliance regimes on this code

Beyond the duty rate, these EU regimes attach to this code. Each verdict follows from the code alone; the goods themselves can still fall outside a regime.

Possible dual-use control codes

Indicative correlation only. The mapping from customs codes to dual-use control codes is guidance, not a classification. Whether an item is controlled depends on its technical parameters.

  • 9A002'Marine gas turbine engines' designed to use liquid fuel and having all of the following, and specially designed assemblies and components therefor:
  • 9A003Specially designed assemblies or components, incorporating any of the "technologies" specified in 9E003.a., 9E003.h. 9E003.i., or 9E003.k, for any of the following aero gas turbine engines:
  • 9A102'Turboprop engine systems' specially designed for unmanned aerial vehicles specified in 9A012 or 9A112.a., and specially designed components therefor, having a 'maximum power' greater than 10 kW.
  • 9A002'Marine gas turbine engines' designed to use liquid fuel and having all of the following, and specially designed assemblies and components therefor:
  • 9A003Specially designed assemblies or components, incorporating any of the "technologies" specified in 9E003.a., 9E003.h. 9E003.i., or 9E003.k, for any of the following aero gas turbine engines:

Derived from TARIC and the published EU regulations. It is a starting point for a screening, not a compliance assessment of your goods.

Binding tariff information for this code

PLBTIWIT-2020-000701Issued by PLValid until 2020-08-03

Rurka doprowadzająca olej do tylnego łożyska turbinowego silnika pomocniczego APS 5000 w samolotach cywilnych. Rurka łączy wydech silnika, w którym umiejscowione jest tylne łożysko ze skrzynią przekładniową, w której znajduje się zespół pomp oleju. Rurka jest zagięta w sześciu miejscach i zakończona z obydwu stron nakrętkami gwintowanymi tzw. B-NUT. Rurka wykonana jest ze stali nierdzewnej. Wymiary: średnica ok. 7 mm, długość w linii prostej ok. 700 mm. Silnik pomocniczy dostarcza energię do rozruchu głównych silników oraz energię elektryczną potrzebną do pracy samolotu na płycie lotniska. Jest również awaryjnym silnikiem w razie awarii silników głównych podtrzymującym pracę najważniejszych urządzeń potrzebnych do bezpiecznego lądowania. Pod względem budowy silnik jest turbiną gazową. .

GB501489167Issued by GBValid until 2019-05-08

METAL SPEED BODY ASSEMBLY. THIS IS PART OF PROBE WHICH MEASURES SPEED IN A PW1000 CIVIL AIRCRAFT GAS TURBINE ENGINE

GB116667068Issued by GBValid until 2013-08-01

PARTS OF A GAS TURBINE ENGINE FOR USE IN CIVIL AIRCRAFT OF AN UNLADEN WEIGHT OF OVER 8000 KG. BEING COMPRESSOR CASINGS.

GB501489853Issued by GBValid until 2013-06-17

SPEED PROBE SUB ASSEMBLY. THIS IS PART OF A PROBE WHICH GOES INTO A TRENT 500 GAS TURBINE USED IN CIVIL AIRCRAFT. THE TOP LEVEL PART MEASURES SPEED IN THE ENGINE.

GB115418591Issued by GBValid until 2012-05-12

BRACKET DESIGNED TO BE FITTED TO A SPECIFIC AIRCRAFT ENGINE. THE BRACKET IS FITTED TO THE EXTERIOR OF THE ENGINE CASING TO RETAIN WIRING LOOM. IT IS MADE FROM INCONEL ALLOY 625 AND MEASURES APPROXIMATELY 41MM X 16MM.

GB115490877Issued by GBValid until 2012-05-12

SPACER DESIGNED TO BE FITTED TO A SPECIFIC AIRCRAFT ENGINE. IT FITS IN THE OUTER CASING ATTACHMENT OF COMPONENTS. IT IS MADE FROM TITANIUM AND MEASURES APPROXIMATELY 49MM X 14MM.

GB115475380Issued by GBValid until 2012-05-10

PLATE BLANKING OUTER, IS FITTED TO THE RB21122B ENGINE WHICH GOES INTO THE BOEING 747-400 CIVIL AIRCRAFT. IT IS MANUFACTURED FROM NICKEL BASED ALLOY. DESIGNED TO BE FITTED TO A SPECIFIC AIRCRAFT ENGINE

GB115412806Issued by GBValid until 2012-05-10

BRACKET LOOP CLAMP GOES INTO THE TURBINE ENGINE FOR AIRBUS SINGLE AISLE CIVIL AIRCRAFT. FITTED TO THE EXTERIOR OF THE ENGINE CASING TO RETAIN PIPE-WORK IN POSITION. MANUFACTURED FROM STAINLESS STEEL. MEASURES APPROXIMATELY 9.0CM BY 6.3CM

Notes that govern this classification

Pos. 8411

Zu Unterposition 8411 99 00: Hierher gehören auch Rotor (Gebläse)-Flügel für Gasturbinen, selbst dann wenn die Gasturbine als Antriebsmaschine kombiniert mit einem elektrischen Generator arbeitet.

Pos. 8411

Einzelentscheidungen zur Kombinierten Nomenklatur (EE) Durchführungsverordnung (EU) Nr. 1035/2014 der Kommission vom 25. September 2014 (ABl. EU Nr. L 287/3) (RV L 1035/14): 1. Ein Turbinenrad aus einer Nickel-Basis-Legierung mit radial angeordneten Schaufeln und zentrischer Nabe zum Aufsatz auf den Wellenverband in einem Abgasturbolader. Das Rad ist derjenige Bestandteil einer Turbine, der die Energie des einströmenden Motorenabgases in eine Drehbewegung zum Antrieb des Verdichterrads des Turboladers umwandelt. Siehe Abbildung 1 Unterposition 8411 99 00 Einreihung gemäß den Allgemeinen Vorschriften 1 und 6 für die Auslegung der Kombinierten Nomenklatur, Anmerkung 2b zu Abschnitt XVI und dem Wortlaut der KN-Positionen 8411 und 8411 99 00. …

Abschnitt XVI

1. Zu Abschnitt XVI gehören nicht: a) Förderbänder und Treibriemen, aus Kunststoffen des Kapitels 39, Förderbänder und Treibriemen aus vulkanisiertem Kautschuk (Position 4010) sowie Waren zu technischen Zwecken aus Weichkautschuk (Position 4016) (RV C1601A00); b) Waren zu technischen Zwecken aus Leder oder rekonstituiertem Leder (Position 4205) oder aus Pelzfellen (Position 4303) (RV C1601B00); c) Spulen, Hülsen, Röhrchen und ähnliche Träger, aus Stoffen aller Art (z. B. Kapitel 39, 40, 44, 48 oder Abschnitt XV) (RV C1601C00); d) Lochkarten für Jacquard- oder ähnliche Maschinen (z. B. Kapitel 39 oder 48 bzw. …

Subdivisions of this code

Frequently asked questions

What does customs tariff code 8411.99.00.10 cover?

Code 8411.99.00.10 covers Of gas turbines, for use in civil aircraft. Classification turns on the material, function, and intended use of the goods, not on their trade name.

What is the duty rate for 8411.99.00.10?

TARIC holds no third-country rate of its own for 8411.99.00.10. The rate follows from the declarable commodity code beneath it.

What is the HS code for 8411.99.00.10?

The first six digits form the HS code: 841199. Those are uniform worldwide, while the further digits carry the EU Combined Nomenclature and the national subdivision.

How many digits does 8411.99.00.10 have?

8411.99.00.10 has ten digits and carries the EU measures held in TARIC. A German import declaration requires the eleven-digit commodity code.

Where does 8411.99.00.10 sit in the tariff?

8411.99.00.10 sits in this hierarchy: 84 NUCLEAR REACTORS, BOILERS, MACHINERY AND MECHANICAL APPLIANCES; PARTS THEREOF > 8411 Turbojets, turbopropellers and other gas turbines > 841199 Other > 84119900 Teile, andere. The parent headings and their notes help decide whether the classification holds.

Is there binding tariff information for 8411.99.00.10?

Yes. The EBTI database holds decisions on 8411.99.00.10, for example PLBTIWIT-2020-000701. A BTI shows which product characteristics the customs authority relied on.

What happens if the customs tariff code is wrong?

An incorrect code leads to post-clearance recovery of duty and import VAT, delays at clearance, and a penalty where it repeats. A classification with documented reasoning can be defended in an audit.

Is 8411.99.00.10 a dual-use item?

The customs code alone does not decide that. An indicative correlation links 8411.99.00.10 to 9A002, 9A003, 9A102, 9A002, 9A003. Whether your item is listed depends on its technical parameters and has to be checked against the wording of the control list.

Does customs tariff code 8411.99.00.10 change?

8411.99.00.10 is currently valid. The Combined Nomenclature is amended every 1 January, so master data should be checked against the current tariff annually.

Read more on classification

Classifying more than one product?

This page shows one code. Zolltarif-Finder classifies entire product lists from Excel, CSV, or your ERP, with reasoning under GRI 1 to 6, official sources, compliance screening, and audit-ready reports.