HS Code 8409100000 80 For aircraft engines

Import trade restrictions for 8409100000 80

This table contains information on trade restrictions for the import of goods into the EU and the EU into third countries. The table contains information on trade restrictions which are imposed due to customs unions, preferences, tariff quotas, customs unions, veterinary controls, third country duties and non-preferential tariff quotas. Our products
	Origin Origin country	Start	Duty / Tax	Legal Legal base Measure type
IR	Iran, Islamic Republic of IR	23/10/2017	Cond: Y cert: Y-966 (29):; Y (09):	Regulation 0267/12 Import control on restricted goods and technologies 711

Explanation of trade restrictions

Erga Omnes means "for all".

Third countries are countries that are not part of the EU.

GSP means "Generalised System of Preferences".

GSP Plus means "Generalised System of Preferences Plus".

European Economic Area (EEA) means all EU member states and Iceland, Liechtenstein and Norway.

OCTs stands for "Overseas Countries and Territories". They are countries and territories that are not part of the EU. More information

CARIFORUM is a regional economic integration organisation comprising 15 Caribbean Community (CARICOM) countries and the Dominican Republic.

SADC EPA stands for "Southern African Development Community - Economic Partnership Agreement".

Duty means "customs duties".

Information

When importing or exporting "For aircraft engines", it is crucial to have the correct HS code or TARIC code. The HS code 8409100000 80 serves as the standard code for this product, ensuring that the appropriate duties and taxes are applied when crossing international borders.

To ensure your business transactions run smoothly when importing or exporting "For aircraft engines", consider the following points:

Inform yourself about the specific import and export regulations in the countries involved. This includes possible restrictions, taxes, and duties applicable to "For aircraft engines".
Check if any additional licenses, permits, or certificates are required to import "For aircraft engines" into the destination country or export it from the country of origin.
Make sure your trading partners have valid identification numbers, such as EORI numbers (Economic Operators Registration and Identification) in the EU, to streamline trade and minimize delays.
Ensure that all trade- and customs-related documents (such as commercial invoices, packing lists, certificates of origin, and insurance policies) are accurately completed and adhere to the respective national regulations.
Keep an eye on the current exchange rates, as well as packaging, shipping, and insurance costs, to accurately calculate trade costs.

In summary, the HS code or TARIC code for "For aircraft engines" is 8409100000 80. Make sure you accurately use this code in all your trade and customs documents to guarantee smooth and hassle-free transactions. With these tips, you'll be better prepared for the challenges of international trade and can successfully import and export "For aircraft engines".

HS Code structure

1. Chapter

There are 21 different sections, which are divided into 96 chapters. Exceptional chapters include chapter 77, which is reserved for future use, chapters 98 and 99, which are limited at national level, and chapter 99, which is a specific code for temporary changes. In the example above, chapter 84 was selected for nuclear reactors, boilers, machinery and mechanical appliances; parts thereof

2. Heading

The heading determines the specific category within a certain chapter. In the example above, the 09 refers to Parts suitable for use solely or principally with the engines of heading|8407|or 8408.

3. Subheading

The last two digits of the international harmonized code are more specific and define subcategories of products. In the example above, the 10 refers to For aircraft engines.

HS Code tree structure

8400000000 80

Chapter NUCLEAR REACTORS, BOILERS, MACHINERY AND MECHANICAL APPLIANCES; PARTS THEREOF

8409000000 80

Parts suitable for use solely or principally with the engines of heading 8407 or 8408

8409100000 80

- For aircraft engines

8409100010 80

- - For engines for use in civil aircraft

8409100020 80

- - Intended to be fitted in aircraft imported duty free or built within the Community

8409100090 80

- - Other

8409910000 10

- Other

8409910000 80

- - Suitable for use solely or principally with spark-ignition internal combustion piston engines

8409910025 80

- - - Air intake module for engine cylinders consisting of: -a suction pipe, -a pressure sensor, -an electric throttle, -hoses, -brackets, for use in the manufacture of engines of motor vehicles

8409910035 80

- - - Fuel distribution pipe complete consisting of rail pipe, high pressure sensor and injectors for direct gasoline fuel injection with: -an operating pressure of not more than 22,5 MPa, -solenoid direct injector, -analog pressure sensor for not more than 22,5 MPa

8409910040 80

- - - Fuel injector with solenoid valve for optimized atomization in the combustion chamber for use in the manufacture of spark-ignition internal combustion piston engines of motor vehicles

8409910045 80

- - - Metal alloy intake and exhaust valve, with a Rockwell hardness HRC 20 or more, for use in the manufacture of spark or compression ignition engines of motor vehicles

8409910050 80

- - - Exhaust manifold with 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

8409910053 80

- - - The exhaust gas recirculation assembly consisting of: -a control unit, -an air throttle, -an intake pipe, -an outlet hose, for use in the manufacture of spark-ignition or compression-ignition combustion engines of motor vehicles

8409910055 80

- - - Nozzle body for the regulation of angle and distribution of fuel injection: -of a cylindrical shape, -made of stainless steel, -with 4 or more, but not more than 16 holes, -with a flow rate of 100 cm³/minute or more, but not more than 500 cm³/minute

8409910070 80

- - - Inlet manifold, exclusively for use in the manufacture of the motor vehicles with: -a width of 40 mm or more but not more than 70 mm, -valves length of 250 mm or more but not more than 350 mm, -air volume of 5,2 litres, and -an electrical flow control system that provides maximum performance at more than 3200 rpm

8409910075 80

- - - Housing of fuel injection valve for generating an electromagnetic field to actuate the injection valve with: -an inlet diameter of 2 mm or more, but not more than 10 mm, -an outlet diameter of 2 mm or more, but not more than 10 mm, -an electric coil with a resistance of 10 Ω or more, but not more than 15 Ω, which ends in an electrical connection, -a plastic covering moulded around a stainless steel tube

8409910080 80

- - - Nozzle needle for opening and closing the flow of fuel in the engine, with: -2 holes, -4 grooves, -a diameter of 3 mm or more, but not more than 6 mm, -a length of 25 mm or more, but not more than 35 mm, -made of stainless steel with hard-chrome plating

8409910085 80

- - - Cylinder head blank for a four cylinder engine with 10 cores, made of aluminium alloy EN AC-45500, with: -no other components, -a hardness of 52 HRB or more, -casting defects size of not more than 0,4 mm and not more than 10 defects per cm², -a dendrite arm space in combustion chamber of not more than 25 μm, -a double deck water jacket design and -a weight of 18 kg or more but not more than 19 kg, -a length of 506 mm or more but not more than 510 mm, -a height of 282 mm or more but not more than 286 mm, -a width of 143,7 mm or more but not more than 144,3 mm, in one single consignment of 1 000 pieces or more

8409910090 80

- - - Other

8409990000 80

- - Other

8409990010 80

- - - Injectors with solenoid valve for optimised atomisation in the engine combustion chamber

8409990025 80

- - - Hoses assembly for fuel return from injectors to engine fuel unit consisting of at least: - three rubber hoses, whether or not with a protective braided sleeving, - three connectors for connecting fuel injectors, - five metal clamps, - one T-shaped plastic joint, for use in the manufacture of engines of motor vehicles

8409990055 80

- - - Exhaust manifold with 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

8409990065 80

8409990070 80