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MINISTRY OF INDUSTRY AND TRADE OF VIETNAM |
SOCIALIST REPUBLIC OF VIETNAM |
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No. 42/2026/TT-BCT |
Hanoi, July 29, 2026 |
CIRCULAR
ON LIST OF DUAL-USE GOODS UNDER JURISDICTION OF THE MINISTRY OF INDUSTRY AND TRADE
Pursuant to Decree No. 40/2025/ND-CP of the Government on functions, tasks, powers, and organizational structures of the Ministry of Industry and Trade amended by Decree No. 109/2025/ND-CP and Decree No. 193/2025/ND-CP;
Pursuant to Decree No. 259/2025/ND-CP of the Government on strategic trade control;
At request of Director of Agency of Foreign Trade;
The Minister of Industry and Trade promulgates Circular on list of dual-use goods under jurisdiction of the Ministry of Industry and Trade.
Article 1. List of dual-use goods under jurisdiction of the Ministry of Industry and Trade
Promulgate List of dual-use goods under jurisdiction of the Ministry of Industry and Trade in service of Clause 2 Article 7 of Decree No. 259/2025/ND-CP under the Appendix attached hereto.
Article 2. Entry into force
1. This Circular comes into force from September 12, 2026.
2. Difficulties that arise during the implementation of this Circular should be reported to the Ministry of Industry and Trade (via Agency of Foreign Trade) in writing./.
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PP. MINISTER Nguyen Sinh Nhat Tan |
APPENDIX
LIST OF DUAL-USE GOODS UNDER JURISDICTION OF THE MINISTRY OF INDUSTRY AND TRADE
(Attached to Circular No. 42/2026/TT-BCT dated July 29, 2026 of the Minister of Industry and Trade)
RULES OF APPLICATION
1. Where only a 4-digit number is listed, all 8-digit numbers contained therein shall also be regulated.
2. Where only a 6-digit number is listed, all 8-digit numbers contained therein shall also be regulated.
3. Where only an 8-digit number is listed, only that number is regulated.
4. Export Control Classification Number (ECCN) of the European Union: is used for reference purposes.
|
No. |
HS code |
Article description |
Technical, technology characteristics |
Reference ECCN |
|
I |
Electronic | |||
|
1 |
85044090 |
High-power direct current power supplies | – Mean static converter having both of the following characteristics:
(i) Capable of continuously producing, over a time period of 8 hours, 100 V or greater with current output of 500 A or greater; (ii) Current or voltage stability better than 0,1% over a time period of 8 hours. – Excluding: Magnet power supplies (high-power, direct current) capable of: continuously producing a current output of 500 A or greater at a voltage of 100 V or greater; a current or voltage regulation better than 0,01% over an 8 hour time period. – Other than the type used in automatic data processors, their units, and telecommunication equipment; other than battery chargers with nominal power above 100 kVA; other than rectifiers; other than inverters. |
3A226 |
|
2 |
85044090 |
High-voltage direct current power supplies | – Mean static converter having both of the following characteristics:
(i) Capable of continuously producing, over a time period of 8 hours, 20 kV or greater with current output of 1 A or greater; (ii) Current or voltage stability better than 0,1% over a time period of 8 hours. – Excluding: High-voltage power supplies for ion sources, having all the following characteristics: capable of continuously operating; voltage output 20.000 V or greater; current output 1A or greater; and voltage stability better than 0,01% over a time period of 8 hours. – Other than the type used in automatic data processors, their units, and telecommunication equipment; other than battery chargers with nominal power above 100 kVA; other than rectifiers; other than inverters. |
3A227 |
|
3 |
85044040 85044090 |
Frequency changers (a.k.a. converters or inverters) | – Mean static converters usable as variable frequency or fixed frequency motor drive and have all of the characteristics below:
(i) Multiphase output providing a power of 40 VA or greater. (ii) Operating at a frequency of 600 Hz or more. (iii) Frequency control better (less) than 0,2%. – Excluding: Frequency changers, including converters or inverters, specially designed or prepared to power motor stator used in gas centrifuge enrichment plant, having both characteristics below: a multiphase output of 600 Hz or greater; high stability (with frequency control better than 0,2%). – Note: Not regulating frequency changers or generators if they are limited in terms of hardware, software, or technology in a way that their capacity is lower than the aforementioned limit. |
3A225 |
|
II |
Chemicals | |||
|
4 |
36020000 |
High explosives or substances or mixtures containing more than 2% by weight thereof | – Other than national defense and security goods.
– crystal density greater than 1,8 g/cm3 and having a detonation velocity greater than 8.000 m/s. |
1C239 |
|
5 |
36020000 |
Shaped charges | ‘Shaped charges’ having all of the following characteristics:
(i) Net Explosive Quantity (NEQ) greater than 90 g; and (ii) Outer casing diameter equal to or greater than 75 mm. |
1A008.a |
|
6 |
36020000 |
Linear shaped cutting charges | Linear shaped cutting charges having all of the following characteristics:
(i) An explosive load greater than 40 g/m; and (ii) A width of 10 mm or more. |
1A008.b |
|
7 |
36031000 36032000 |
Detonating cord | Detonating cord with explosive core load greater than 64 g/m |
1A008.c |
|
8 |
36036000 |
Electrically driven explosive detonators | – Including:
(i) Exploding bridge (EB); (ii) Exploding bridge wire (EBW); (iii) Slapper; (iv) Exploding foil initiators (EFI). Note: – All regulated electrically driven explosive detonators utilize a small electrical conductor (bridge, bridge wire, or foil) that explosively vaporizes when a fast, high-current electrical pulse is passed through it. – In non slapper types, the exploding conductor starts a chemical detonation in a contacting high explosive material such as PETN (pentaerythritoltetranitrate). – In slapper detonators, the explosive vaporization of the electrical conductor drives a flyer or slapper across a gap, and the impact of the slapper on an explosive starts a chemical detonation. The slapper in some designs is driven by magnetic force. – The term exploding foil detonator may refer to either an EB or a slapper-type detonator. |
1A007.b |
|
9 |
29214400 |
2-Nitrodiphenylamine | CAS 119-75-5 |
1C111.c |
|
10 |
29209000 |
Triethylene glycol dinitrate | CAS 111-22-8 |
1C111.c |
|
11 |
29209000 |
Trimethylolethane trinitrate | CAS 3032-55-1 |
1C111.c |
|
12 |
29209000 |
Diethylene glycol dinitrate | CAS 693-21-0 |
1C111.c |
|
13 |
28500000 |
Hydrides of phosphorus, arsenic, or antimony with high purity | Having a purity better than 99,999%, even diluted in inert gases or hydrogen.
Excluding hydrides containing 20% molar or more of inert gases or hydrogen. |
3C004 |
|
14 |
29319090 |
(iv) Organo-metallic compounds of aluminum, gallium, or indium with high purity | Organo-metallic compounds of aluminum, gallium, or indium that have a chemical purity (on metal basis) greater than 99,999%. |
3C003.a |
|
15 |
29314400 29314800 293149 29315200 29315300 29315400 293159 29319049 |
Organo-arsenic, organo-antimony, and organo-phosphorus compounds with high purity. | Organo-arsenic, organo-antimony, and organo-phosphorus compounds that have a chemical purity (on inorganic element basis) greater than 99,999%. |
3C003.b |
|
16 |
39269099 |
Syntactic foam designed for underwater use at marine depths not exceeding 1.000 meters and a density less than 561 kg/m3 | Syntactic foam consists of hollow spheres of plastic or glass bound together in a matrix material of plastic.
(i) Designed for underwater use at marine depth not exceeding 1.000 m; and (ii) Of a density less than 561 kg/m3. |
8C001 |
|
III |
Metal, alloy | |||
|
17 |
81041900 81049000 |
High strength magnesium alloy | – Having both the following characteristics:
(i) A tensile strength of 345 MPa or more; and (ii) A corrosion rate of less than 1 mm/year in 3% sodium chloride aqueous solution measured in accordance with ASTM standard G-31 or national equivalents. – Other than the type used in base cladding – Magnesium metal, by weight percentage, is greater than any other element in the alloy. – Made from metal alloy powder or particulate material, having all of the following: Mg-Al-X or Mg-X-Al; where X stands for one or multiple alloy parts. |
1C002.b |
|
18 |
75022000 75051200 75052200 75062000 75071200 7508 |
High strength nickel alloy | – Having any of the following:
(i) A ‘stress-rupture life’ of 10.000 hours or longer at 923 K (650 °C) at a stress of 676 MPa; or (ii) A ‘low cycle fatigue life’ of 10.000 cycles or more at 823 K (550 °C) at a maximum stress of 1.095 MPa; – Where: “Stress-rupture life” should be measured in accordance with ASTM standard E-139 or national equivalents; “Low cycle fatigue life” should be measured in accordance with ASTM Standard E-606 or national equivalents. – Other than the type used in base cladding – Nickel metal, by weight percentage, is greater than any other element in the alloy. – Made from metal alloy powder or particulate material, having all of the following: Nickel alloys (Ni-Al-X, Ni-X-Al) qualified for turbine engine “parts” or “components,” i.e., with less than 3 non-metallic particles (introduced during the manufacturing process) larger than 100 µm in 109 alloy particles; where X stands for one or multiple alloy parts. |
1C002.b |
|
19 |
81082000 81089000
|
High strength titanium alloy | – Having any of the following:
(i) A ‘stress-rupture life’ of 10.000 hours or longer at 723 K (450 °C) at a stress of 200 MPa; or (ii) A ‘low cycle fatigue life’ of 10.000 cycles or more at 723 K (450 °C) at a maximum stress of 400 MPa. – Where: “Stress-rupture life” should be measured in accordance with ASTM standard E-139 or national equivalents; “Low cycle fatigue life” should be measured in accordance with ASTM Standard E-606 or national equivalents. – Other than the type used in base cladding – Titanium metal, by weight percentage, is greater than any other element in the alloy. – Made from metal alloy powder or particulate material, having all of the following: Ti-Al-X or Ti-X-Al; where X stands for one or multiple alloy parts. |
1C002.b |
|
20 |
76012000 760429 76052100 76052910 76052990 76061290 76069200 76082000 76169990 |
High strength aluminum alloy | – Having any of the following:
(i) A tensile strength of 240 MPa or more at 473 K (200 °C); (ii) A tensile strength of 415 MPa or more at 298 K (25 °C); – Other than the type used in base cladding – Aluminum metal, by weight percentage, is greater than any other element in the alloy. – Made from metal alloy powder or particulate material, having all of the following: Al-Mg-X or Al-X-Mg, Al-Zn-X or Al-X-Zn, Al-Fe-X or Al-X-Fe; where X stands for one or multiple alloy parts. |
1C002.b |
|
21 |
72253090 72254090 72255090 72259190 72259990 72269190 72269290 72269999 73041900 730451 730459 73049090 73065099 73069097 73069099 |
Maraging steel | – Maraging steels are iron alloys that are generally characterized by high nickel, very low carbon content not exceed 0,03% in weight, use substitutional elements or precipitates to produce strengthening and age-hardening of the alloy. Maraging steel is subjected to heat treatment cycles to facilitate the martensitic transformation process (solution annealed stage) and subsequently age hardened (precipitation hardened stage).
– Maraging steels usable in “missile” (complete missile system and unmanned aerial vehicle system capable of achieving a range equal to or greater than 300 km), as follows: (i) Having an ultimate tensile strength, measured at 293K (20 °C), equal to or greater than 0,9 GPa in the solution annealed stage; or 1,5 GPa in the precipitation hardened stage; (ii) Any of the following forms: – Sheet, plate or tubing with a wall or plate thickness equal to or less than 5,0 mm; or – Tubular forms with a wall thickness equal to or less than 50 mm and having an inner diameter equal to or greater than 270 mm. |
1C116 |
|
22 |
72181000 72191400 72192400 72193300 72193400 72193500 72199000 72210000 72221100 72221900 722220 722230 73041100 730422 730424 73044100 73044900 73053110 730611 73062100 73064019 73064020 |
Stainless steel of which titanium content is greater than 0,1%, nickel 4,5 – 7%, and chromium 17 – 23%. | Titanium-stabilized duplex stainless steel (Ti-DSS) having all of the following characteristics:
(i) Containing 17,0 – 23,0% by weight of chromium and 4,5 – 7,0% by weight of nickel; (ii) Having a titanium content of greater than 0,1% by weight; and (iii) A ferritic-austenitic microstructure (also referred to as a two-phase microstructure) of which at least 10% by volume (according to ASTM E-1181-87 or national equivalents) is austenite; and (iv) Having any of the following forms: – Ingots or bars having a size of 100 mm or more in each dimension; – Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or – Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less. |
1C118 |
|
23 |
81019990 |
Tungsten, tungsten carbide, and alloys containing more than 90% tungsten by weight, having both of the following characteristics | – Having both of the following characteristics:
(i) In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; and (ii) A mass greater than 20 kg. – Excluding manufactures specially designed as weights or gamma-ray collimators. – Excluding materials usable in parts of “missile” (complete missile system and unmanned aerial vehicle system capable of achieving a range equal to or greater than 300 km), as follows: (i) Tungsten and alloys in particulate form with a tungsten content of 97% by weight or more and a particle size of 50 × 10−6 m (50 µm) or less; (ii) Tungsten materials in the solid form having all of the following: + Any of the following material compositions: Tungsten and alloys containing 97% by weight or more of tungsten; Copper infiltrated tungsten containing 80% by weight or more of tungsten; Silver infiltrated tungsten containing 80% by weight or more of tungsten; and + Able to be machined to any of the following products: Cylinders having a diameter of 120 mm or greater and a length of 50 mm or greater; Tubes having an inner diameter of 65 mm or greater and a wall thickness of 25 mm or greater and a length of 50 mm or greater; or Blocks having a size of 120 mm × 120 mm × 50 mm or greater |
1C226 |
|
24 |
81021000 81029900 |
Molybdenum and high molybdenum alloy | Molybdenum and alloys in particulate form with a molybdenum content of 97% by weight or more and a particle size of 50 × 10−6 m (50 µm) or less |
1C117.b |
|
25 |
810610 |
High purity bismuth | Having both of the following characteristics:
(i) A purity of 99,99% or greater by weight; and (ii) Containing less than 10 parts per million by weight of silver. |
1C229 |
|
26 |
81041100 81041900 81043000 81049000 |
High purity Magnesium | Having both of the following characteristics:
(i) Containing less than 200 parts per million by weight of metallic impurities other than calcium; and (ii) Containing less than 10 parts per million by weight of boron. |
1C228 |
|
27 |
28051200 |
High purity calcium | Having both of the following characteristics:
(i) Containing less than 1.000 parts per million by weight of metallic impurities other than magnesium; and (ii) Containing less than 10 parts per million by weight of boron. |
1C227 |
|
28 |
81123100 81123900 |
Hafnium and hafnium alloys | Hafnium metal, hafnium alloys and compounds containing more than 60% hafnium by weight |
1C231 |
|
29 |
81121200 81121300 81121900 |
Beryllium and beryllium alloys | Beryllium metal, alloys containing more than 50% beryllium by weight, beryllium compounds, manufactures thereof, and waste or scrap of any of the foregoing.
Other than: (i) Metal windows for X-ray machines, or for bore-hole logging devices; (ii) Oxide shapes in fabricated or semi-fabricated forms “specially designed” for electronic component parts or as substrates for electronic circuits (iii) Beryl (silicate of beryllium and aluminum) in the form of emeralds or aquamarines. |
1C230 |
|
30 |
81124100 81124900 |
Rhenium and rhenium alloys | Rhenium and alloys containing rhenium having both of the following characteristics:
(i) Alloys containing 90% by weight or more of rhenium; or 90% by weight or more of any combination of rhenium and tungsten. (ii) A mass greater than 20 kg and in forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 mm and 300 mm. |
1C241 |
|
IV |
Unmanned aerial vehicles | |||
|
31 |
8806 |
Unmanned aerial vehicles (UAV) | Designed to have controlled flight out of the direct “natural vision” of the “operator” and having any of the following:
(i) A minimum sustained flight of 1 hour; or (ii) A minimum sustained flight of 30 minutes or higher and design to take off and maintain in stable flight during wind gust of 46,3 km/h (25 knot) or higher. Where: – “Operator” means the person who activates or controls the UAV flight. – “Natural vision” means unaided human sight, with or without corrective lenses. – Endurance is to be calculated for ISA conditions (ISO 2533:1975) at sea level in zero wind. |
9A012 |
