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EAEU HS code

8807 30 000 0 — Parts of goods of heading 8801, 8802 or 8806: other parts of aeroplanes, helicopters or unmanned aircraft

Parts of goods of heading 8801, 8802 or 8806: other parts of aeroplanes, helicopters or unmanned aircraft

Names come in English where the EU Combined Nomenclature publishes them — chapters, headings and subheadings, whose first six digits are the same Harmonized System; deeper EAEU detail is a machine translation, marked as such. Official texts — tariff notes, measures, lists and classification rulings — are the original: customs and your broker go by that wording. Where we show a machine translation of them, it is marked; where our quality check rejected one, the Russian stays.

Machine translation. The original is the Russian text of the EAEU tariff, and customs goes by it; this translation is for understanding only and has no legal force.

Duty rate
0%

This is the base rate. A tariff quota, a preference for the country of origin and a tariff exemption lower it; anti-dumping and special duties are paid on top of it

EEC Council Decision No. 80 of 14.09.2021

Supplementary unit
Not applicable
Requirements and measures
14

None: mandatory labelling, recycling fee, conformity assessment, EAEU non-tariff regulation, trade defence measures — duty on top of the tariff, tariff quota.

Whether a measure applies to your goods depends on their characteristics and the shipping documents

VAT
22%

The general import rate in Russia: Tax Code of Russia, Art. 164(3) (Federal Law No. 425-FZ of 28.11.2025). This code is not named on the 10% VAT list (Decree No. 908) or the exemption list (No. 1042). The list of medical goods No. 688 is not checked here.

Product reference in Word (in Russian)

Duties, taxes, fees, bans, permits and controls in one free file.

Import into Russia

Import reference

Export from Russia

Export reference

Import into Russia

Payments on import

Duty for this code: 0%. On top of the duty, on import into Russia you pay VAT of 22% of the customs value including the duty (Article 160 of the Tax Code) and the customs processing fee — a fixed amount by value band. Customs value: the price of the goods, delivery to the border, local costs.

CCT rate: the EAEU CCT as amended by Решение Совета ЕЭК № 80 от 14.09.2021, from 01.01.2022; our register has no later decisions on the rate for this code.

How the rate for this code has changed
Customs fee scale by customs value, 2026
  • from 0 to 200,000 ₽1,231 ₽
  • from 200,000 to 450,000 ₽2,462 ₽
  • from 450,000 to 1,200,000 ₽4,924 ₽
  • from 1,200,000 to 2,700,000 ₽13,541 ₽
  • from 2,700,000 to 4,200,000 ₽18,465 ₽
  • from 4,200,000 to 5,500,000 ₽21,344 ₽
  • from 5,500,000 to 10,000,000 ₽49,240 ₽
  • over 10,000,000 ₽73,860 ₽

Fee per declaration. Russian Government Resolution No. 1637 of 28.11.2024 as amended by Resolution No. 1638 of 23.10.2025.

Import VAT in EAEU countries

  • Russia22%
  • Kazakhstan16%
  • Belarus20%
  • Armenia20%
  • Kyrgyzstan12%

Standard rate; each country has reduced rates and exemptions for some goods. The duty for the code above is the union one, the same for all

Customs declaration fee

  • Kazakhstan6 MCI per goods declaration, KZT 25,950 in 2026
  • BelarusBYN 120 for goods of chapter 88from Jan 1, 2027: BYN 135
  • ArmeniaAMD 3,500 for clearanceinspection and recording: AMD 1,000 per consignment up to 1 t and AMD 300 per each additional tonne
  • Kyrgyzstan0.4% of the customs valuenot less than 5 and not more than 2,500 calculation units
Calculate the whole deal →Quick payment calculation →

Tariff preferences

The code is on the EAEU list of preferential goods: for goods originating in a beneficiary country the duty is lower

Least developed countrieszero rate0%
46 countries

Burkina Faso, Guinea, Eritrea, Congo - Kinshasa, Timor-Leste, Afghanistan, Mauritania, Yemen, Cambodia, Lesotho, Laos, Bangladesh, Nepal, Tanzania, Palestinian Territories, Angola, Benin, Burundi, Haiti, Gambia, Guinea-Bissau, Djibouti, Zambia, Kiribati, Liberia, Madagascar, Malawi, Mali, Mozambique, Niger, Rwanda, Senegal, Myanmar (Burma), Sudan, Sierra Leone, Uganda, Chad, South Sudan, Syria, Solomon Islands, Comoros, Togo, Tuvalu, Ethiopia, Somalia, Central African Republic

The preference requires a document of origin and compliance with the direct consignment rule; customs checks the right to it at declaration.

Documents required

A summary across all the lists we check: the document, its legal basis and whether it covers the whole code. Details are in the sections below.

Our lists contain no documents or permits for importing this code.

Export ban

applies to goods bought in that country or from its companies

  • EUРегламент Совета ЕС № 833/2014, приложение XL (приоритетные товары)
  • USAПравила экспортного контроля США (EAR), часть 746, дополнение № 4 (промышленные товары)

Goods in customs transit may be tracked with a navigation seal: this depends on the route and procedure, not on the code (EAEU Agreement of 19.04.2022, EEC Board Decision No. 84).

Customs declaration hints

Boxes 33, 36, 44, 47

Which codes go into the boxes of the goods declaration for this product. The codes come from the classifiers of Customs Union Commission Decision No. 378. Reliefs, document types and excise depend on the shipment, so such lines carry a condition.

Box 33 · Commodity code

  • 8807300000
  • Оin the second subdivision, if goods with different names are declared under one code

Box 36 · Preference

  • ОООО-ООFees, duty, excise, VAT: no relief claimed, no excise (dash)
  • ООНН-ООТарифная преференция в отношении товаров, происходящих из наименее развитых стран · if the goods originate in a least developed country and origin is proven

Box 44 · Documents produced

  • 06013Сертификат о происхождении товара формы "А" · if the goods are imported under a tariff preference

Box 47 · Calculation of payments

  • 1010Таможенные сборы за совершение таможенных операций (за таможенное оформление товаров, за таможенное декларирование товаров, за таможенные операции)
  • 2010Ввозная таможенная пошлина (иные пошлины, налоги и сборы, имеющие эквивалентное действие), обязанность по уплате которой возникла с 1 сентября 2010 г.
  • 5010Налог на добавленную стоимость

Completion rules and classifiers: Решение Комиссии Таможенного союза от 20.05.2010 № 257; классификаторы — Решение Комиссии Таможенного союза от 20.09.2010 № 378

Each requirement in detailVeterinary, plant quarantine and sanitary control · How it is certified

Veterinary, plant quarantine and sanitary control

Goods fall under supervision by their type and characteristics

  • Sanitary and epidemiological supervision (control)

    rule for the whole chapter 88
    Иная продукция (товары), в отношении которой одним из государств – членов Евразийского экономического союза введены временные санитарные меры

    The list names this code with “ex”: control applies only to goods with this description.

    Решение Коллегии Евразийской экономической комиссии от 17.09.2019 № 154

How it is certified

Valid documents in the EAEU unified register for subheading 8807 30: certificates 0, declarations 14.

By technical regulation
ТР ТС 020/201111ТР ЕАЭС 037/20163ТР ТС 004/20113ТР ТС 010/20111
Schemes
1д132д1The letter after the scheme number shows the form: certification or declaration of conformity.
Most active certification bodies
НП РУП «Белорусский государственный институт стандартизации и сертификации»
Manufacturers outside the EAEU
China7Hong Kong SAR China1

Manufacturers of these goods →Check a supplier’s document by its number →

Export from Russia

Documents required

A summary across all the lists we check: the document, its legal basis and whether it covers the whole code. Details are in the sections below.

Customs declaration hints

Boxes 33, 44, 47

Which codes go into the boxes of the goods declaration for this product. The codes come from the classifiers of Customs Union Commission Decision No. 378. Reliefs, document types and excise depend on the shipment, so such lines carry a condition.

Box 33 · Commodity code

  • 8807300000
  • Оin the second subdivision, if goods with different names are declared under one code

Box 44 · Documents produced

  • 01011Лицензия на экспорт и (или) импорт товаров · Постановление Правительства РФ от 09.03.2022 № 312
  • 01151Лицензия, перечень (приложение) к лицензии на ввоз (вывоз) товаров, подлежащих экспортному контролю, выданные уполномоченным государственным органом государств - членов Евразийского экономического союза · Постановление Правительства РФ от 19.07.2022 № 1299, пункты 1.1.1.1, 9.1.12.2, 8.1.6.3 и другие
  • 01153Разрешение (подтверждение) на ввоз (вывоз) товаров, подлежащих экспортному контролю, выданное уполномоченным государственным органом государств - членов Евразийского экономического союза в области экспортного контроля · Постановление Правительства РФ от 19.07.2022 № 1299, пункты 1.1.1.1, 9.1.12.2, 8.1.6.3 и другие
  • 01154Заключение (идентификационное), выдаваемое в соответствии с законодательством в области экспортного контроля государств - членов Евразийского экономического союза, о непринадлежности товаров к товарам, включенным в единые списки контролируемых товаров и технологий · if the goods are not on the control lists

Box 47 · Calculation of payments

  • 1010Таможенные сборы за совершение таможенных операций (за таможенное оформление товаров, за таможенное декларирование товаров, за таможенные операции)

Completion rules and classifiers: Решение Комиссии Таможенного союза от 20.05.2010 № 257; классификаторы — Решение Комиссии Таможенного союза от 20.09.2010 № 378

Russian bans and restrictions

May apply

Whether a measure applies to your goods is determined by the provisos in the “code” column. Measures are taken from the register as of the date the act was published; the act is named on every line

  • 8807 (за исключением 8807 90 000)Out of RussiaProhibited

    Отдельные виды товаров — временный запрет на вывоз

    Части летательных аппаратов товарной позиции 8801, 8802 или 8806

    Постановление Правительства РФ от 09.03.2022 № 311 — until Dec 31, 2027

  • 8807 30 000 0Out of RussiaPermit required

    Транспортные средства, их части и комплектующие

    Прочие части самолетов, вертолетов или беспилотных летательных аппаратов

    Постановление Правительства РФ от 09.03.2022 № 312 — until Dec 31, 2027

  • 8807 (за исключением 8807 10 000 0, 8807 20 000 0, 8807 30 000 0, 8807 90 000)Out of RussiaPermit requiredThe code is named in an exception

    Read the proviso in full: the exception may depend on what the goods are for.

    Промышленная продукция

    Части летательных аппаратов товарной позиции 8801, 8802, 8806

    Постановление Правительства РФ от 09.03.2022 № 312 — until Dec 31, 2027

  • 8479 89 970 1 8479 89 970 7 8807 30 000 0Out of RussiaProhibited

    Товары двойного назначения

    воздушные стартеры

    Countries: Австралия, Албания, Андорра, Багамские Острова, Великобритания, государства — члены ЕС, Исландия, Канада, Лихтенштейн, Микронезия, Монако, Новая Зеландия, Норвегия, Республика Корея, Сан-Марино, Северная Македония, Сингапур, США, Тайвань, Украина, Черногория, Швейцария, Япония

    Постановление Правительства РФ от 09.03.2022 № 313 — until Dec 31, 2027

  • 8483 10 210 8 8483 10 500 0 8483 10 950 0 8483 40 230 8 8807 30 000 0Out of RussiaProhibited

    Товары двойного назначения

    элементы трансмиссии, включая редукторы и редукторные рамы, валы и тормоза несущего винта

    Countries: Австралия, Албания, Андорра, Багамские Острова, Великобритания, государства — члены ЕС, Исландия, Канада, Лихтенштейн, Микронезия, Монако, Новая Зеландия, Норвегия, Республика Корея, Сан-Марино, Северная Македония, Сингапур, США, Тайвань, Украина, Черногория, Швейцария, Япония

    Постановление Правительства РФ от 09.03.2022 № 313 — until Dec 31, 2027

  • 8411 91 000 8413 30 200 8 8413 30 800 8 8413 50 400 0 8413 50 690 0 8413 50 800 0 8413 60 390 0 8479 89 970 7 8807 30 000 0 9032 20 000 0Out of RussiaProhibited

    Товары двойного назначения

    элементы топливной и гидравлической систем: насосы и насосы-регуляторы; автоматы разгрузки насосов; топливные регуляторы; гидроаккумуляторы

    Countries: Австралия, Албания, Андорра, Багамские Острова, Великобритания, государства — члены ЕС, Исландия, Канада, Лихтенштейн, Микронезия, Монако, Новая Зеландия, Норвегия, Республика Корея, Сан-Марино, Северная Македония, Сингапур, США, Тайвань, Украина, Черногория, Швейцария, Япония

    Постановление Правительства РФ от 09.03.2022 № 313 — until Dec 31, 2027

  • 4016 99 970 8 8807 30 000 0Out of RussiaProhibited

    Товары двойного назначения

    баки топливные

    Countries: Австралия, Албания, Андорра, Багамские Острова, Великобритания, государства — члены ЕС, Исландия, Канада, Лихтенштейн, Микронезия, Монако, Новая Зеландия, Норвегия, Республика Корея, Сан-Марино, Северная Македония, Сингапур, США, Тайвань, Украина, Черногория, Швейцария, Япония

    Постановление Правительства РФ от 09.03.2022 № 313 — until Dec 31, 2027

  • 8407 10 000 2 8411 11 000 9 8411 12 8526 10 000 8806 8807 9007 10 000 0 9014 10 000 0 9014 20 200 9 9014 20 800 9014 80 000 0 9306 90Out of RussiaProhibited

    Товары двойного назначения

    Беспилотные летательные аппараты и их части

    Countries: Австралия, Албания, Андорра, Багамские Острова, Великобритания, государства — члены ЕС, Исландия, Канада, Лихтенштейн, Микронезия, Монако, Новая Зеландия, Норвегия, Республика Корея, Сан-Марино, Северная Македония, Сингапур, США, Тайвань, Украина, Черногория, Швейцария, Япония

    Постановление Правительства РФ от 09.03.2022 № 313 — until Dec 31, 2027

Export control

Expert review needed

Goods fall under control by their technical characteristics, regardless of the code. Supplying without a licence when one is required is a criminal offence

  • Товары и технологии двойного назначения (вооружение и военная техника)

    Постановление Правительства РФ от 19.07.2022 № 1299

    Раздел 1 · Категория 1. Специальные материалы и связанные с ними оборудование и снаряжение

    • Системы, оборудование и компоненты → Компоненты, изготовленные из фторированных соединений:1.1.1.1 Уплотнения, прокладки, уплотнительные материалы или топливные баки, специально разработанные для использования в летательных или аэрокосмических аппаратах и изготовленные из материалов, содержащих более 50 процентов (по весу) любого материала, определенного в пункте 1.3.9.1 или 1.3.9.2;

    Раздел 1 · Категория 9. Авиационно-космическая промышленность и двигательные/силовые установки

    • Системы, оборудование и компоненты → Беспилотные (воздушные) летательные аппараты (БЛА) или беспилотные дирижабли, взаимосвязанные системы, оборудование и компоненты:9.1.12.2 Взаимосвязанные оборудование и компоненты:

    Раздел 4 · вывоз по соображениям национальной безопасности · Категория 8. Транспортные средства

    • Системы, оборудование и компоненты → Запасные части и комплектующие изделия для вертолетов с максимальным взлетным весом более 4500 кг:8.1.6.3 Элементы систем запуска, управления и охлаждения двигателей, указанных в пункте 8.1.6.1: а) воздушные стартеры; б) агрегаты зажигания и автоматы пуска двигателя; в) электронные регуляторы двигателя; г) вентиляторы; д) автоматические панели пуска; е) блоки автоматического регулирования и контроля;
    Show 2 more
    • 8.1.6.6 Элементы системы управления и пилотажно-навигационного оборудования: а) комбинированные агрегаты управления (гидроусилители); б) рулевые агрегаты (системы); в) автопилоты; г) бортовые вычислительные комплексы; д) многофункциональные пульты управления; е) высотомеры, включая корректоры высоты и приемопередатчики высотомеров; ж) авиагоризонты, включая малогабаритные гировертикали; з) курсовая аппаратура, включая радиокомпасы, гироагрегаты, пульты управления, компасы магнитные, механизмы коррекционные, блоки ориентации и индикации и доплеровские измерители скорости и сноса; и) аппаратура автоматической регистрации параметров полета, включая блоки сбора полетной информации и регистраторы речевой информации; к) бортовая аппаратура речевых сообщений; л) системы аварийной предупреждающей и уведомляющей сигнализации, включая блоки контроля и блоки аварийно-предупреждающих и уведомляющих сигналов;
    • 8.1.6.7 Элементы топливной и гидравлической систем: а) насосы и насосы-регуляторы; б) автоматы разгрузки насосов; в) топливные регуляторы; г) баки топливные; д) гидроаккумуляторы;

The code has been checked against the export control lists: 6 of 6 (Russian Government Decrees No. 1284–1288 of 16.07.2022 and No. 1299 of 19.07.2022).

Classification

Where it sits in the nomenclature

Section XVII. Vehicles, aircraft, vessels and associated transport equipment

  1. 88Aircraft, spacecraft, and parts thereof
  2. 8807 30 000 0you are here

Notes to chapter 88 — Aircraft, spacecraft, and parts thereof 6 items

Note

Machine translation. The original is the Russian text of the EAEU tariff, and customs goes by it; this translation is for understanding only and has no legal force.

1. For the purposes of this Chapter, the expression “unmanned aircraft” means any aircraft other than those referred to in heading 8801 designed to fly without a pilot on board. Such vehicles may be designed to carry payloads or equipped with stationary digital cameras or other equipment to enable them to perform utilitarian functions during flight.

The expression “unmanned aircraft”, however, does not include flying toys intended solely for entertainment (heading 9503).

Subheading notes

English text as published in Annex I to Regulation (EU) 2021/1832 (Combined Nomenclature). The EAEU tariff and the EU nomenclature copy these notes from the same convention. For a Russian declaration the binding version is the Russian one: Annex to Decision No 80 of the EEC Council of 14 September 2021.

1. For the purposes of subheadings 8802 11 to 8802 40, the expression ‘unladen weight’ means the weight of the machine in normal flying order, excluding the weight of the crew and of fuel and equipment other than permanently fitted items of equipment.

2. For the purposes of subheadings 8806 21 to 8806 24 and 8806 91 to 8806 94, the expression ‘maximum take-off weight’ means the maximum weight of the machine in normal flying order, at take-off, including the weight of payload, equipment and fuel.

Additional notes of the Eurasian Economic Union

Machine translation. The original is the Russian text of the EAEU tariff, and customs goes by it; this translation is for understanding only and has no legal force.

1. For the purpose of subheading 8802 40 00, the term “maximum take-off mass” means the corresponding mass specified by the manufacturer in the flight manual of the aircraft.

2. For the purposes of positions 8802 30 000 3, 8802 40 00, the term “cargo ramp” means a device forming part of the structure of the aircraft connecting the interior space of the aircraft and the surface of the ground with an accessible slope for the transport (entry/exit) of goods into and out of the interior space of the aircraft.

3. In heading 8802:

(a) the term wide-body aircraft means aircraft having a maximum outer width of the fuselage (excluding protruding parts, for example for landing gear) of at least 5 m;

(б) термин «самолеты дальнемагистральные» означает самолеты, способные без дополнительных топливных баков, с максимальной предусмотренной нагрузкой и без дозаправки, совершать беспосадочные полеты на расстояние не менее 8000 км для пассажирских самолетов и на расстояние не менее 6000 км для грузовых самолетов;

(c) the term "two aisles between rows of seats" means that the cabin in which the largest number of seats is accommodated has two through aisles from the beginning to the end of the cabin.

Classification rulings for this code (20)

Machine translation from Russian. The original is the Russian wording of the ruling, and customs goes by it; this translation is for understanding only and has no legal force.

The rear upper panel of the passenger cabin is a decorative panel 120 cm wide, 80 cm long at the rear of the ceiling and 90 cm high on the upper part of the rear wall of the passenger cabin of the helicopter with a box 115 cm wide, 42 cm deep, 40 cm high fixed on it.

Full description

The panel is made by vacuum infusion (impregnation of fiberglass with epoxy resin under the influence of vacuum in the form) followed by metalworking and tightening with artificial leather. The panel is mounted with screws (not included in the delivery) from the bottom to the design of the helicopter fuselage and the rear lower panel of the passenger cabin interior system, as well as from the top left / right to the left and right ceiling side panels of the passenger cabin interior system. The panel performs a decorative function, representing a decorative element of finishing the passenger cabin, improves the appearance of the passenger cabin of the helicopter.

On the upper part of the panel, two holes are made, through which ducts are mounted and air supply tubes from the air conditioning system are connected. The panel is packed in a wooden box.

GRI 1 and 6

The central upper panel of the passenger cabin is a rectangular, with a slight bend, decorative panel 121 cm wide, 103 cm long and 6 cm high.

Full description

The panel is made by vacuum infusion (impregnation of fiberglass with epoxy resin under the influence of vacuum in the form) followed by metalworking and tightening with artificial leather. On the panel there are 13 holes on the left and right sides for the screws (not included in the supply), a total of 26 holes, through which the central upper panel is attached to the previously installed upper side panels (not included in the supply), having specially provided for installation of response technological holes. The panel performs a decorative function, representing a decorative element of finishing the ceiling of the passenger cabin of the helicopter, improves the appearance of the passenger cabin of the helicopter.

On the central upper panel of the passenger cabin there are two holes measuring 120 mm by 60 mm, through which air ducts are mounted and air supply tubes from the air conditioning system are connected. The panel is packed in a wooden box.

GRI 1 and 6

The panel of the swing door of the passenger cabin on the left is a lining on the inner surface of the left door of the passenger cabin of the helicopter.

Full description

The panel is made by vacuum infusion (impregnation of fiberglass with epoxy resin under the influence of vacuum in the form) with subsequent metalworking and tightening of artificial and natural leather in the color of the interior of the helicopter. The panel has a complex volumetric geometric shape, which corresponds to the shape of the inner surface of the door of the passenger cabin of the helicopter. The panel is mounted on the inner surface of the door by means of eight brackets (not included in the delivery), which, on the one hand, are pre-installed on the inner surface of the door, and on the other hand, by means of eight screws (not included in the delivery) are attached to eight specially provided for installation of technological holes on the panel.

The panel performs a decorative function, representing a decorative element of finishing the passenger cabin, improving the appearance of the inner surface of the left door of the passenger cabin. The panel is the basis for placing stickers (not included in the delivery) with the designation of emergency exit, emergency actions and door handle control, and also hides the door lock mechanism (not included in the delivery kit). The panel has a hole with a diameter of 17.5 ± 2.5 mm under the door handle and the following overall dimensions: length - 1282 mm, width - 980 mm, depth in different parts of the product - 140-210 mm.

The panel is packed in a wooden box.

GRI 1 and 6

The panel of the swing door of the passenger cabin on the right is a lining on the inner surface of the right door of the passenger cabin of the helicopter.

Full description

The panel is made by vacuum infusion (impregnation of fiberglass with epoxy resin under the influence of vacuum in the form) with subsequent metalworking and tightening of artificial and natural leather in the color of the interior of the helicopter. The panel has a complex volumetric geometric shape, which corresponds to the shape of the inner surface of the door of the passenger cabin of the helicopter. The panel is mounted on the inner surface of the door by means of eight brackets (not included in the delivery), which, on the one hand, are pre-installed on the inner surface of the door, and on the other hand, by means of eight screws (not included in the delivery) are attached to eight specially provided for installation of technological holes on the panel.

The panel performs a decorative function, representing a decorative element of finishing the passenger cabin, improving the appearance of the interior surface of the right door of the passenger cabin. The panel is the basis for placing stickers (not included in the delivery) with the designation of emergency exit, emergency actions and door handle control, and also hides the door lock mechanism (not included in the delivery kit). The panel has a hole with a diameter of 17.5 ± 2.5 mm under the door handle and the following overall dimensions: length - 1282 mm, width - 980 mm, depth in different parts of the product - 140-210 mm.

The panel is packed in a wooden box.

GRI 1 and 6

The panel of the pilot's door on the right is a lining on the inner surface of the right door of the helicopter pilot.

Full description

The panel is made of sheet plastic, reinforced with fiberglass, and has a complex volumetric geometric shape, which corresponds to the shape of the inner surface of the door of the helicopter pilot. The panel is mounted on the inner surface of the door by means of seven screws (not included in the package), which are installed in seven specially provided for installation of response technological holes. The panel performs a decorative function, representing a decorative element of the cockpit decoration of the helicopter pilots, transforming the appearance of the inner surface of the right door of the pilot, is the basis for placing stickers (not included in the delivery kit) with the designation of the emergency exit and the control scheme for the handle of the pilot's door, and also hides the mechanism of the pilot's door lock (not included in the delivery kit).

The panel has a cut hole under the door handle and the following dimensions: length - 472 mm, width of the narrow part - 120 mm, width of the wide part - 187 mm, maximum depth - 25 mm. The panel is packed in a protective film and placed in an individual place in a foam bed, which is nested in a wooden box.

GRI 1 and 6

The panel of the pilot's door on the left is a lining on the inner surface of the left door of the helicopter pilot.

Full description

The panel is made of sheet plastic, reinforced with fiberglass, and has a complex volumetric geometric shape, which corresponds to the shape of the inner surface of the door of the helicopter pilot. The panel is mounted on the inner surface of the door by means of seven screws (not included in the package), which are installed in seven specially provided for installation of response technological holes. The panel performs a decorative function, representing a decorative element of finishing the cockpit of helicopter pilots, transforming the appearance of the inner surface of the left door of the pilot, is the basis for placing stickers (not included in the delivery kit) with the designation of the emergency exit and the control scheme for the handle of the pilot's door, and also hides the mechanism of the pilot's door lock (not included in the delivery kit).

The panel has a cut hole under the door handle and the following dimensions: length - 472 mm, width of the narrow part - 120 mm, width of the wide part - 187 mm, maximum depth - 25 mm. The panel is packed in a protective film and placed in an individual place in a foam bed, which is nested in a wooden box.

GRI 1 and 6

The side panel front lower right is a decorative skin of the front lower surface of the wall of the passenger cabin of a civil helicopter under the starboard window.

Full description

The panel has a complex volumetric geometric shape with overall dimensions: 940 mm (length) x 460 mm (width), maximum thickness of 235 mm. The panel in the lower part has a rectangular hole measuring 420 mm (length) x 130 mm (width) for the installation of the ventilation grille (not included in the delivery), as well as in the central part a ledge with three clothing buttons - the place of attachment of the lower right seat lining (not included in the delivery). The panel is made by vacuum infusion (impregnation of carbon fiber fabric with epoxy resin under the influence of vacuum in the form) with subsequent finishing: metalworking and natural skin tightening.

The panel is mounted with seven screws (not included in the delivery) along with a ventilation grille to the inner surface of the right wall and one screw (not included in the delivery) to the doorway of the passenger cabin of the helicopter. Holes for screws are provided on the panel. In the process of installation, a sheet of noise insulation material is glued to the inner surface of the panel (not included in the delivery kit). The panel performs a decorative function, is a decorative element of finishing the passenger cabin, improves the appearance of the inner surface of the passenger cabin wall under the starboard window, and also provides safe and comfortable transportation of passengers, reducing noise in the cabin of the helicopter.

The panel is packed in a wooden box.

GRI 1 and 6

The main gearbox of the helicopter is designed to transfer torque from the engines (not included in the delivery kit) to the shafts of the carrier and steering screws and provides drive auxiliary units of the helicopter.

Full description

The main gearbox consists of the following main components: body of the main gearbox assembled from aluminum alloy, free-range coupling - 2 pcs, front thrust mounting - 2 pcs, rear thrust mounting - 2 pcs, baseboard, planetary gear, conical gear - 8 pcs, shaft connecting - 2 pcs, shaft adapter under the brake disc, gearbox output shaft, rotor shaft, the input shaft of the gearbox - 2 pcs, rotor-sleeve skewer the thrust of the skewed machine, rotor-driven coupling assembly, drive unit, hinge joints for rotor blades, lubrication system of the main gearbox, warning system for the presence of chips, hydraulic system, rotor braking device.

The main technical parameters: the frequency of rotation of the input shafts of the gearbox - 21 000 rpm, the frequency of rotation of the rotor shaft - 296 rpm, the frequency of rotation of the output shaft of the gearbox - 4532 rpm. The main gearbox is attached to the power frames of the fuselage with a frame that transmits to the fuselage the forces and moments perceived by the gearbox.

GRI 1 and 6

The rear lower panel is a decorative sheathing of the rear lower surface of the wall of the passenger cabin of a civilian helicopter between the passenger cabin and the luggage compartment.

Full description

The panel has a rectangular shape with overall dimensions: 1650 mm (length) x 440 mm (width), maximum thickness of 140 mm. The panel is equipped with two rectangular holes measuring 620 mm (length) x 50 mm (width) for the installation of two ventilation grilles (not included in the package). The panel is made by vacuum infusion (impregnation of carbon fiber fabric with epoxy resin under the influence of vacuum in the form) with subsequent finishing: metalworking and natural skin tightening. The panel is mounted with seven screws (not included in the delivery), of which: three screws to the rear inner surface of the passenger cabin wall and four screws (two screws to the right and left) to the side panel of the rear lower left and to the side panel of the rear lower right passenger cabin of the helicopter.

Holes for screws are provided on the panel. In the process of installation, two ventilation grilles are installed on the front surface of the panel. The panel performs a decorative function, representing a decorative element of finishing the passenger cabin, improves the appearance of the inner surface of the wall of the passenger cabin of the helicopter. The panel is packed in a wooden box.

GRI 1 and 6

The fuel system of the helicopter is designed to accommodate the necessary amount of fuel for the flight and its supply to the engines in all flight modes.

Full description

The fuel system includes the following main subsystems: a subsystem of fuel tanks, a subsystem of fuel supply pipeline and drainage tubes, a subsystem of fuel drainage tubes and a ceiling panel for controlling the supply of fuel to engines. The fuel reserve is located in two main fuel tanks located in the left and right parts of the fuselage of the helicopter, as well as in an additional tank located in the cargo compartment. Fuel supply to engines from fuel tanks is carried out using fuel pumps through the pipes of the subsystem of the fuel pipeline.

To ensure the cavitation-free operation of the fuel pumps, to ensure minimum internal and external pressures on the walls of the tanks, to regulate the air pressure in the tanks during their fueling and draining, drainage of fuel tanks is provided. Drainage is carried out by supplying air fuel tanks to the superfuel space, which equalizes the air pressure inside the tanks with atmospheric pressure. The air is fed through a subsystem of drainage tubes. In addition, with the help of drainage tubes, water condensate formed on the fuel system is drained.

Fuel discharge from the tanks is carried out through the subsystem of drainage tubes. The fuel system is supplied unassembled and consists of the following main components: pumps, fuel tanks, rubber hoses, fuel and drainage pipes.

GRI 1, 2(a) and 6

The product is designed to control the position of the rotor helicopter.

Full description

The rotor of the helicopter (not included in the supply) is associated with the control system through a distortion machine (not included in the supply), with the help of which the control system transfers outgoing movements (movements) to the rotor. Control of the rotor of the helicopter performs two tasks, one of which is to control the overall pitch of the rotor, the other in controlling the cyclic pitch. Control of the total pitch of the rotor blades is to change the installation angle of all the rotor blades, which is carried out with the simultaneous rotation of them in the axial hinge relative to the longitudinal axis of the blade by means of levers and control rods.

With a simultaneous increase in the angle of installation of all blades, the helicopter rises, while reducing the angles of installation of all blades, the helicopter descends. Control of the cyclic pitch of the rotor blades is a sinusoidal change in the angles of installation of the rotor blades in the axial hinge relative to the ground plane and the appearance of the horizontal component of the rotor thrust, which causes the forward movement of the helicopter in a given direction. Control of the cyclic pitch of the blades is carried out by means of levers of the cyclic control of the screw, thrusts of control, supports of control levers.

The product consists of the following main components, which during assembly form a single mechanical unit: control levers, control traction, tubes for torque transmission, supports of control levers. Delivered in disassembled form.

GRI 1, 2(a) and 6

The side panel of the rear lower right is a decorative skin of the rear lower surface of the wall of the passenger cabin of the civil helicopter under the starboard window.

Full description

The panel has a complex volumetric geometric shape with overall dimensions: 895 mm (length) x 430 mm (width), maximum thickness of 140 mm. The panel in the lower left corner has a rectangular hole measuring 52 mm x 43 mm under the socket and a decorative aluminum alloy cover, which is attached to the panel by means of a latch and closes the above hole. The panel is made by vacuum infusion (impregnation of carbon fiber fabric with epoxy resin under the influence of vacuum in the form) with subsequent finishing: metalworking and natural skin tightening.

The panel is mounted with three screws (not included in the delivery) to the side inner surface of the right wall and the rear panel of the passenger cabin of the helicopter. Holes for screws are provided on the panel. In the process of installation, a sheet of noise insulation material is glued to the inner surface of the panel (not included in the delivery kit). The panel performs a decorative function, is a decorative element of finishing the passenger cabin, improves the appearance of the inner surface of the passenger cabin wall under the rear window of the starboard side, and also provides safe and comfortable transportation of passengers, reducing noise in the cabin of the helicopter.

The panel is packed in a wooden box.

GRI 1 and 6

The steering rotor control system is a pedal unit, which is used to manually control the pilot of the helicopter's flight path (course control).

Full description

The control system is supplied in an unassembled form and consists of the following main components: rockers assembled (...), bushings - 2 pcs., pedals assembled - 2 pcs., traction assembled (...), thrust of controls assembled (...), regulating thrust assembly, pedal switches - 4 pcs., plate pads - 4 pcs., washer - 4 pcs., balancing lever. The route control body of the helicopter is the steering rotor (not included in the package). The steering screw is controlled by changing the overall pitch of its blades using foot control pedals.

Acting on the pedals, the pilot through the system of levers and thrusts can, by means of leashes, turn simultaneously all the blades of the steering screw around their longitudinal axis, increasing or decreasing the pitch of the screw, depending on which direction and how much the pedals were moved.

GRI 1, 2(a) and 6

The tail beam of the helicopter is a structural element of the helicopter, is a metal monocoque structure in the form of a truncated cone and consists of skin, beams and frames.

Full description

The design of the tail beam also includes the following main elements: tail stabilizer (left and right sides of the tail stabilizer are two wings with different angles of inclination), fairing edge and tail gear fairings (front and rear). The end of the tail beam is made in the form of a keel. The tail beam is connected to the central part of the fuselage of the helicopter through a flange joint using bolts (not included in the package).

GRI 1 and 6

The side panel front lower left is a decorative skin of the front lower surface of the wall of the passenger cabin of a civil helicopter under the window of the left side.

Full description

The panel has a complex volumetric geometric shape with overall dimensions: 940 mm (length) x 460 mm (width), maximum thickness of 235 mm. The panel in the lower part has a rectangular hole measuring 420 mm (length) x 130 mm (width) for the installation of the ventilation grille (not included in the delivery), as well as in the central part a ledge with three clothing buttons - the place of attachment of the lower left seat lining (not included in the delivery). The panel is made by vacuum infusion (impregnation of carbon fiber fabric with epoxy resin under the influence of vacuum in the form) with subsequent finishing: metalworking and natural skin tightening.

The panel is mounted with seven screws (not included in the delivery) along with a ventilation grille to the inner surface of the left wall and one screw (not included in the delivery) to the doorway of the passenger cabin of the helicopter. Holes for screws are provided on the panel. In the process of installation, a sheet of noise insulation material is glued to the inner surface of the panel (not included in the delivery kit). The panel performs a decorative function, is a decorative element of finishing the passenger cabin, improves the appearance of the inner surface of the passenger cabin wall under the left side window, and also provides safe and comfortable transportation of passengers, reducing noise in the cabin of the helicopter.

The panel is packed in a wooden box.

GRI 1 and 6

The side panel of the rear lower left is a decorative skin of the rear lower surface of the wall of the passenger cabin of the civil helicopter under the window of the left side.

Full description

The panel has a complex volumetric geometric shape with overall dimensions: 895 mm (length) x 430 mm (width), maximum thickness of 140 mm. The panel in the lower right corner has a rectangular hole measuring 52 mm x 43 mm under the socket and a decorative aluminum alloy cover, which is attached to the panel by means of a latch and closes the above hole. The panel is made by vacuum infusion (impregnation of carbon fiber fabric with epoxy resin under the influence of vacuum in the form) with subsequent finishing: metalworking and natural skin tightening.

The panel is mounted with three screws (not included in the delivery) to the side inner surface of the left wall and the rear panel of the passenger cabin of the helicopter. Holes for screws are provided on the panel. In the process of installation, a sheet of noise insulation material is glued to the inner surface of the panel (not included in the delivery kit). The panel performs a decorative function, is a decorative element of finishing the passenger cabin, improves the appearance of the inner surface of the passenger cabin wall under the rear window of the left side, and also provides safe and comfortable transportation of passengers, reducing noise in the cabin of the helicopter.

The panel is packed in a wooden box.

GRI 1 and 6

The upper right side panel of the passenger cabin with a swing door is a lining on the inner surface of the wall of the passenger cabin of the right side of the helicopter.

Full description

The panel is made by vacuum infusion (impregnation of fiberglass with epoxy resin under the influence of vacuum in the form) followed by metalworking and tightening with artificial leather. The panel has a complex volumetric geometric shape, which corresponds to the shape of the surface of the wall of the passenger cabin on the right side of the helicopter. The panel is mounted with four screws with washers to the brackets (not included in the delivery), installed on the side inner surface of the wall of the passenger cabin of the helicopter.

Specially provided for installation of technological holes for screws are provided on the panel. The panel performs a decorative function, representing a decorative element of finishing the passenger cabin, improving the appearance of the inner surface of the wall of the passenger cabin on the right side of the helicopter. The panel has two holes measuring 730 x 500 mm for the installation of two windows of the passenger cabin (not included in the package). The panel has the following overall dimensions: length - 2600 mm, width - 970 mm, depth in different parts of the product - 140-520 mm.

The panel is packed in a wooden box.

GRI 1 and 6

The left upper side panel of the passenger cabin with a swing door is a lining on the inner surface of the wall of the passenger cabin of the left side of the helicopter.

Full description

The panel is made by vacuum infusion (impregnation of fiberglass with epoxy resin under the influence of vacuum in the form) followed by metalworking and tightening with artificial leather. The panel has a complex volumetric geometric shape, which corresponds to the shape of the surface of the wall of the passenger cabin on the left side of the helicopter. The panel is mounted with four screws with washers to the brackets (not included in the delivery), installed on the side inner surface of the wall of the passenger cabin of the helicopter.

Specially provided for installation of technological holes for screws are provided on the panel. The panel performs a decorative function, representing a decorative element of finishing the passenger cabin, improving the appearance of the inner surface of the wall of the passenger cabin on the left side of the helicopter. The panel has two holes measuring 730 x 500 mm for the installation of two windows of the passenger cabin (not included in the package). The panel has the following overall dimensions: length - 2600 mm, width - 970 mm, depth in different parts of the product - 140-520 mm.

The panel is packed in a wooden box.

GRI 1 and 6

The front upper panel of the passenger cabin is a rectangular, with a slight bend in the front, decorative panel 121 cm wide, 76 cm long and 12 cm high.

Full description

On the panel there is a pad width of 47 cm, length of 58 cm, height of 1 cm, which is attached to the panel on "Velcro". The panel and the lining are made by vacuum infusion (impregnation of fiberglass with epoxy resin under the influence of vacuum in the form) followed by metalworking and tightening with artificial leather. On the panel there are 10 holes on the left and right sides for screws (not included in the supply), a total of 20 holes, through which the front upper panel is attached to the previously installed upper side panels (not included in the supply), having specially provided for installation of response technological holes.

The panel performs a decorative function, representing a decorative element of the decoration of the passenger cabin of the helicopter, improves the appearance of the passenger cabin of the helicopter. On the front upper panel of the passenger cabin there are two holes with a diameter of 75 mm, closed with a lining. The holes are intended for possible laying of additional cables or installation of ducts. The panel is packed in a wooden box.

GRI 1 and 6

The partition is installed in the cabin of the helicopter between the cockpit and the passenger cabin.

Full description

The partition has a complex geometric shape and is attached to the fuselage of the helicopter by means of five brackets made of aluminum alloy: three in the lower part of the partition and two on the sides. The brackets installed on the partition are fixed with screws: two screws for each lower bracket and four screws for each side bracket. The brackets are installed on the partition during its assembly. On the sides of the partition there are fastening places in the form of embedded bushings with internal threads for connecting the interior panels of the helicopter (not included in the delivery kit).

The partition is made of a cellular sandwich panel, which consists of two facing plates of fiberglass impregnated with epoxy resin and a cellular aggregate made of aramid paper impregnated with fire-resistant phenolic resin. Cladding plates and cellular aggregate are fastened with epoxy resin. The partition has a combined upholstery (natural and artificial leather) and a sliding window with organic glass. The window opening is closed with a decorative fiberglass lining. On the decorative lining on the side of the passenger cabin, an aluminum alloy bar and two aluminum alloy brackets for mounting the side panels are fixed (not included in the delivery kit).

From the side of the cockpit, a fiberglass pocket is installed on the partition, covered with natural leather. The partition has the following overall dimensions: length - 1830 mm, width 1310 mm, thickness - 35 mm.

GRI 1 and 6

EEC decisions on this code

Rates, trade defence measures, licensing and classification: decisions since 2016 whose text names code 8807300000.

Titles of acts are given in Russian as published: this is how they are cited in customs documents.

  • Duties and rates

    Решение Коллегии ЕЭК № 1

    О применении ставок ввозных таможенных пошлин в отношении товаров, происходящих из Исламской Республики Иран и ввозимых на таможенную территорию Евразийского экономического союза, и о признании утратившими силу некоторых решений Коллегии Евразийской экономической комиссии

    adopted Jan 14, 2025 · published Jan 17, 2025 · entered into force May 15, 2025

    Text of the act (opens in a new tab)
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