Legalize / European Union / Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restrictive measures against Iran and repealing Regulation (EU) No 961/2010 / History

Reform history

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restrictive measures against Iran and repealing Regulation (EU) No 961/2010

39 versions · 2012-03-23

2025-09-30

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2025-07-29

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2024-09-13

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2024-07-30

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2023-10-18

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2023-10-11

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2023-04-26

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2023-04-04

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2022-06-29

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2022-04-13

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2021-07-31

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

Changes on 2021-07-31

@@ -429,7 +429,7 @@

### **CATEGORY 0 — NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT**

### **0A** Systems, Equipment and Components

#### **0A** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.12/Part 1 (1) | | |

| --- | --- | --- | --- |

@@ -582,7 +582,7 @@

### **CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT**

### **1A** Systems, Equipment and Components

#### **1A** Systems, Equipment and Components

| --- | --- | --- | --- |

@@ -593,7 +593,7 @@

| 1A226 | Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics: a. Made of phosphor bronze mesh chemically treated to improve wettability; and b. Designed to be used in vacuum distillation towers. | 4.A.1. | Specialized packings which may be used in separating heavy water from ordinary water, having both of the following characteristics: a. Made of phosphor bronze mesh chemically treated to improve wettability; and b. Designed to be used in vacuum distillation towers. |

| 1A227 | High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor: a. A ‘cold area’ greater than 0,09 m2; b. A density greater than 3 g/cm3; and c. A thickness of 100 mm or greater. *Technical Note:* *In 1A227 the term ‘cold area’ means the viewing area of the window exposed to the lowest level of radiation in the design application.* | 1.A.1. | High-density (lead glass or other) radiation shielding windows, having all of the following characteristics, and specially designed frames therefor: a. A ‘cold area’ greater than 0,09 m2; b. A density greater than 3 g/cm3; and c. A thickness of 100 mm or greater. *Technical Note:* *In Item 1.A.1.a. the term ‘cold area’ means the viewing area of the window exposed to the lowest level of radiation in the design application.* |

### **1B** Test, Inspection and Production Equipment

#### **1B** Test, Inspection and Production Equipment

| --- | --- | --- | --- |

@@ -608,7 +608,7 @@

| 1B233 | Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows: a. Facilities or plants for the separation of lithium isotopes; b. Equipment for the separation of lithium isotopes based on the lithium-mercury amalgam process, as follows: 1. Packed liquid-liquid exchange columns specially designed for lithium amalgams; 2. Mercury or lithium amalgam pumps; 3. Lithium amalgam electrolysis cells; 4. Evaporators for concentrated lithium hydroxide solution; c. Ion exchange systems specially designed for lithium isotope separation, and specially designed components therefor; d. Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers), specially designed for lithium isotope separation, and specially designed components therefor. | 2.B.2. | Lithium isotope separation facilities or plants, and systems and equipment therefor, as follows: N.B.: Certain lithium isotope separation equipment and components for the plasma separation process (PSP) are also directly applicable to uranium isotope separation and are controlled under INFCIRC/254 Part 1 (as amended). a. Facilities or plants for the separation of lithium isotopes; b. Equipment for the separation of lithium isotopes based on the lithium-mercury amalgam process, as follows: 1. Packed liquid-liquid exchange columns specially designed for lithium amalgams; 2. Mercury or lithium amalgam pumps; 3. Lithium amalgam electrolysis cells; 4. Evaporators for concentrated lithium hydroxide solution; c. Ion exchange systems specially designed for lithium isotope separation, and specially designed component parts therefor; d. Chemical exchange systems (employing crown ethers, cryptands, or lariat ethers) specially designed for lithium isotope separation, and specially designed component parts therefor. |

| 1B234 | High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics: N.B.: SEE ALSO MILITARY GOODS CONTROLS. a. Designed to fully contain an explosion equivalent to 2 kg of TNT or greater; and b. Having design elements or features enabling real time or delayed transfer of diagnostic or measurement information. | 5.B.7. | High explosive containment vessels, chambers, containers and other similar containment devices designed for the testing of high explosives or explosive devices and having both of the following characteristics: a. Designed to fully contain an explosion equivalent to 2 kg of TNT or greater; and b. Having design elements or features enabling real time or delayed transfer of diagnostic or measurement information. |

### **1C** Materials

#### **1C** Materials

| --- | --- | --- | --- |

@@ -636,14 +636,14 @@

| 1C240 | Nickel powder and porous nickel metal, other than those specified in 0C005, as follows: a. Nickel powder having both of the following characteristics: 1. A nickel purity content of 99,0 % or greater by weight; and 2. A mean particle size of less than 10 μm measured by American Society for Testing and Materials (ASTM) B330 standard; b. Porous nickel metal produced from materials specified in 1C240.a. *Note:* *1C240 does not control the following:* *a.* *Filamentary nickel powders;* *b.* *Single porous nickel sheets with an area of 1 000 cm2 per sheet or less.* *Technical Note:* *1C240.b. refers to porous metal formed by compacting and sintering the materials in 1C240.a. to form a metal material with fine pores interconnected throughout the structure.* | 2.C.16. | Nickel powder and porous nickel metal, as follows: N.B.: For nickel powders which are especially prepared for the manufacture of gaseous diffusion barriers see INFCIRC/254/Part 1 (as amended). a. Nickel powder having both of the following characteristics: 1. A nickel purity content of 99,0 % or greater by weight; and 2. A mean particle size of less than 10 μm measured by the ASTM B 330 standard; b. Porous nickel metal produced from materials specified in Item 2.C.16.a. Note: Item 2.C.16. does not control the following: a. Filamentary nickel powders; b. Single porous nickel metal sheets with an area of 1 000 cm2 per sheet or less. Technical Note: Item 2.C.16.b. refers to porous metal formed by compacting and sintering the material in Item 2.C.16.a. to form a metal material with fine pores interconnected throughout the structure. |

| 1C241 | Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, other than those specified in 1C226, having both of the following characteristics: a. In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; and b. A mass greater than 20 kg. | 2.C.20. | Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys of rhenium and tungsten containing 90 % by weight or more of any combination of rhenium and tungsten, having both of the following characteristics: a. In forms with a hollow cylindrical symmetry (including cylinder segments) with an inside diameter between 100 and 300 mm; and b. A mass greater than 20 kg. |

### **1D** Software

#### **1D** Software

| --- | --- | --- | --- |

| 1D001 | “Software” specially designed or modified for the “development”, “production” or “use” of equipment specified in 1B001 to 1B003. | 1.D.2. | “software” means a collection of one or more “programs” or “microprograms” fixed in any tangible medium of expression |

| 1D201 | “Software” specially designed for the “use” of goods specified in 1B201. | 1.D.3. | “software” means a collection of one or more “programs” or “microprograms” fixed in any tangible medium of expression |

### **1E** Technology

#### **1E** Technology

| --- | --- | --- | --- |

@@ -653,14 +653,14 @@

### **CATEGORY 2 — MATERIALS PROCESSING**

### **2A** Systems, Equipment and Components

#### **2A** Systems, Equipment and Components

| --- | --- | --- | --- |

| 2A225 | Crucibles made of materials resistant to liquid actinide metals, as follows: a. Crucibles having both of the following characteristics: 1. A volume of between 150 cm3 and 8 000 cm3; and 2. Made of or coated with any of the following materials, or combination of the following materials, having an overall impurity level of 2 % or less by weight: a. Calcium fluoride (CaF2); b. Calcium zirconate (metazirconate) (CaZrO3); c. Cerium sulphide (Ce2S3); d. Erbium oxide (erbia) (Er2O3); e. Hafnium oxide (hafnia) (HfO2); f. Magnesium oxide (MgO); g. Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W); h. Yttrium oxide (yttria) (Y2O3); or i. Zirconium oxide (zirconia) (ZrO2); b. Crucibles having both of the following characteristics: 1. A volume of between 50 cm3 and 2 000 cm3; and 2. Made of or lined with tantalum, having a purity of 99,9 % or greater by weight; c. Crucibles having all of the following characteristics: 1. A volume of between 50 cm3 and 2 000 cm3; 2. Made of or lined with tantalum, having a purity of 98 % or greater by weight; and 3. Coated with tantalum carbide, nitride, boride, or any combination thereof. | 2.A.1 | Crucibles made of materials resistant to liquid actinide metals, as follows: a. Crucibles having both of the following characteristics: 1. A volume of between 150 cm3 (150 ml) and 8 000 cm3 (8 l (litres)); and 2. Made of or coated with any of the following materials, or combination of the following materials, having an overall impurity level of 2 % or less by weight: a. Calcium fluoride (CaF2); b. Calcium zirconate (metazirconate) (CaZrO3); c. Cerium sulfide (Ce2S3); d. Erbium oxide (erbia) (Er2O3); e. Hafnium oxide (hafnia) (HfO2); f. Magnesium oxide (MgO); g. Nitrided niobium-titanium-tungsten alloy (approximately 50 % Nb, 30 % Ti, 20 % W); h. Yttrium oxide (yttria) (Y2O3); or i. Zirconium oxide (zirconia) (ZrO2); b. Crucibles having both of the following characteristics: 1. A volume of between 50 cm3 (50 ml) and 2 000 cm3 (2 liters); and 2. Made of or lined with tantalum, having a purity of 99,9 % or greater by weight; c. Crucibles having all of the following characteristics: 1. A volume of between 50 cm3 (50 ml) and 2 000 cm3 (2 liters); 2. Made of or lined with tantalum, having a purity of 98 % or greater by weight; and 3. Coated with tantalum carbide, nitride, boride, or any combination thereof. |

| 2A226 | Valves having all of the following characteristics: a. A ‘nominal size’ of 5 mm or greater; b. Having a bellows seal; and c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight. *Technical Note:* *For valves with different inlet and outlet diameters, the ‘nominal size’ in 2A226 refers to the smallest diameter.* | 3.A.3. | Valves having all of the following characteristics: a. A nominal size of 5 mm or greater; b. Having a bellows seal; and c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel alloy containing more than 60 % nickel by weight. *Technical Note:* *For valves with different inlet and outlet diameter, the nominal size parameter in Item 3.A.3.a. refers to the smallest diameter.* |

### **2B** Test, Inspection and Production Equipment

#### **2B** Test, Inspection and Production Equipment

| --- | --- | --- | --- |

@@ -692,7 +692,7 @@

| 2B233 | Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following: **N.B.:** **SEE ALSO 2B350.i.** a. Capable of an inlet volume flow rate of 50 m3/h or greater; b. Capable of a pressure ratio of 2:1 or greater; and c. Having all surfaces that come in contact with the process gas made from any of the following materials: 1. Aluminium or aluminium alloy; 2. Aluminium oxide; 3. Stainless steel; 4. Nickel or nickel alloy; 5. Phosphor bronze; or 6. Fluoropolymers. | 3.A.9. | Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum pumps having all of the following characteristics: a. Capable of an inlet volume flow rate of 50 m3/h or greater; b. Capable of a pressure ratio of 2:1 or greater; and c. Having all surfaces that come in contact with the process gas made from any of the following materials: 1. Aluminium or aluminium alloy; 2. Aluminium oxide; 3. Stainless steel; 4. Nickel or nickel alloy; 5. Phosphor bronze; or 6. Fluoropolymers. Technical Notes: 1. In a scroll compressor or vacuum pump, crescent-shaped pockets of gas are trapped between one or more pairs of intermeshed spiral vanes, or scrolls, one of which moves while the other remains stationary. The moving scroll orbits the stationary scroll; it does not rotate. As the moving scroll orbits the stationary scroll, the gas pockets diminish in size (i.e., they are compressed) as they move toward the outlet port of the machine. 2. In a bellows-sealed scroll compressor or vacuum pump, the process gas is totally isolated from the lubricated parts of the pump and from the external atmosphere by a metal bellows. One end of the bellows is attached to the moving scroll and the other end is attached to the stationary housing of the pump. 3. Fluoropolymers include, but are not limited to, the following materials: a. Polytetrafluoroethylene (PTFE), b. Fluorinated Ethylene Propylene (FEP), c. Perfluoroalkoxy (PFA), d. Polychlorotrifluoroethylene (PCTFE); and e. Vinylidene fluoride-hexafluoropropylene copolymer. |

| (1) Manufacturers calculating positioning accuracy in accordance with ISO 230/2 (1997) or (2006) should consult the competent authorities of the Member State in which they are established. | | | |

### **2D** Software

#### **2D** Software

| --- | --- | --- | --- |

@@ -702,7 +702,7 @@

| 2D201 | “Software” specially designed for the “use” of equipment specified in 2B204, 2B206, 2B207, 2B209, 2B219 or 2B227. | 1.D.1. | “Software” specially designed or modified for the “use” of equipment specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7. Note: “Software” specially designed or modified for systems specified in Item 1.B.3.d. includes “software” for simultaneous measurements of wall thickness and contour. |

| 2D202 | “Software” specially designed or modified for the “development”, “production” or “use” of equipment specified in 2B201. *Note:* *2D202 does not control part programming “software” that generates “numerical control” command codes but does not allow direct use of equipment for machining various parts.* | 1.D.2. | “Software” specially designed or modified for the “development”, “production”, or “use” of equipment specified in Item 1.B.2. Note: Item 1.D.2. does not control part programming “software” that generates “numerical control” command codes but does not allow direct use of equipment for machining various parts. |

### **2E** Technology

#### **2E** Technology

| --- | --- | --- | --- |

@@ -713,7 +713,7 @@

### **CATEGORY 3 — ELECTRONICS**

### **3A** Systems, Equipment and Components

#### **3A** Systems, Equipment and Components

| --- | --- | --- | --- |

@@ -731,14 +731,14 @@

| 3A233 | Mass spectrometers, other than those specified in 0B002.g., capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor: a. Inductively coupled plasma mass spectrometers (ICP/MS); b. Glow discharge mass spectrometers (GDMS); c. Thermal ionization mass spectrometers (TIMS); d. Electron bombardment mass spectrometers having both of the following features: 1. A molecular beam inlet system that injects a collimated beam of analyte molecules into a region of the ion source where the molecules are ionized by an electron beam; and 2. One or more ‘cold traps’ that can be cooled to a temperature of 193 K (–80 °C); e. Not used; f. Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides. *Technical Notes:* *1.* *Electron bombardment mass spectrometers in 3A233.d. are also known as electron impact mass spectrometers or electron ionization mass spectrometers.* *2.* *In 3A233.d.2., a ‘cold trap’ is a device that traps gas molecules by condensing or freezing them on cold surfaces. For the purposes of 3A233.d.2., a closed-loop gaseous helium cryogenic vacuum pump is not a ‘cold trap’.* | 3.B.6. | Mass spectrometers capable of measuring ions of 230 atomic mass units or greater and having a resolution of better than 2 parts in 230, as follows, and ion sources therefor: N.B.: Mass spectrometers especially designed or prepared for analyzing on-line samples of uranium hexafluoride are controlled under INFCIRC/254/Part 1 (as amended). a. Inductively coupled plasma mass spectrometers (ICP/MS); b. Glow discharge mass spectrometers (GDMS); c. Thermal ionization mass spectrometers (TIMS); d. Electron bombardment mass spectrometers having both of the following features: 1. A molecular beam inlet system that injects a collimated beam of analyte molecules into a region of the ion source where the molecules are ionized by an electron beam; and 2. One or more cold traps that can be cooled to a temperature of 193 K (–80 °C) or less in order to trap analyte molecules that are not ionized by the electron beam; e. Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides. |

| 3A234 | Striplines to provide low inductance path to detonators with the following characteristics: a. Voltage rating greater than 2 kV; and b Inductance of less than 20 nH. | 6.A.6. | Striplines to provide low inductance path to detonators with the following characteristics: a. Voltage rating greater than 2 kV; and b. Inductance of less than 20 nH. |

### **3D** Software

#### **3D** Software

| --- | --- | --- | --- |

| 3D002 | “Software” specially designed for the “use” of equipment specified in 3B001.a. to f., 3B002 or 3A225 | 3.D.1. | “Software” specially designed for the “use” of equipment specified in Items 3.A.1., 3.B.3. or 3.B.4. |

| 3D225 | “Software” specially designed to enhance or release the performance of frequency changers or generators to meet the characteristics of 3A225. | 3.D.3. | “Software” specially designed to enhance or release the performance characteristics of equipment controlled in Item 3.A.1. |

### **3E** Technology

#### **3E** Technology

| --- | --- | --- | --- |

@@ -748,7 +748,7 @@

### **CATEGORY 6 — SENSORS AND LASERS**

### **6A** Systems, Equipment and Components

#### **6A** Systems, Equipment and Components

| --- | --- | --- | --- |

@@ -773,13 +773,13 @@

| 6A226 | Pressure sensors, as follows: a. Shock pressure gauges capable of measuring pressures greater than 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene bifluoride (PVBF, PVF2); b. Quartz pressure transducers for pressures greater than 10 GPa. | 5.B.5.b. | b. Shock pressure gauges capable of measuring pressures greater than 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene bifluoride (PVBF, PVF2); |

| 5.B.5.c. | c. Quartz pressure transducers for pressures greater than 10 GPa. Note: Item 5.B.5.a. includes velocity interferometers such as VISARs (Velocity Interferometer Systems for Any Reflector), DLIs (Doppler Laser Interferometers) and PDV (Photonic Doppler Velocimeters) also known as Het-V (Heterodyne Velocimeters). | | |

### **6D** Software

#### **6D** Software

| --- | --- | --- | --- |

| 6D203 | “Software” specially designed to enhance or release the performance of cameras or imaging devices to meet the characteristics of 6A203.a. to 6A203.c. | 5.D.2. | “Software” or encryption keys/codes specially designed to enhance or release the performance characteristics of equipment controlled in Item 5.B.3. |

### **6E** Technology

#### **6E** Technology

| --- | --- | --- | --- |

@@ -820,7 +820,7 @@

4.Controls on “technology” transfer do not apply to information “in the public domain”, to “basic scientific research” or to the minimum necessary information for patent applications.

### II.A. **GOODS**

#### II.A. **GOODS**

| A0. Nuclear Materials, Facilities, and Equipment | | |

| --- | --- | --- |

@@ -930,7 +930,7 @@

| II.A9.002 | ‘Load Cells’ capable of measuring rocket motor thrust having a capacity exceeding 30 kN. Technical Note: ‘Load Cells’ means devices and transducers for the measurement of force in both tension and in compression. Note: II.A9.002 does not include equipment, devices or transducers, specially designed for the measurement of the weight of vehicles, e.g. weigh bridges. | 9B117 |

| II.A9.003 | Electrical power generation gas turbines, components and related equipment as follows: (a) Gas Turbines specially designed for electrical power generation, having an output exceeding 200 MW; (b) Vanes, Stators, Combustion Chambers and Fuel Injection Nozzles, specially designed for electrical power generation gas turbines specified in II.A9.003.a; (c) Equipment specially designed for the “development” and “production” of electrical power generation gas turbines specified in II. A9.003.a. | 9A001 9A002 9A003 9B001 9B003 9B004 |

### II.B. **TECHNOLOGY**

#### II.B. **TECHNOLOGY**

| No | Description | Related item from Annex I to Regulation (EC) No 428/2009 |

| --- | --- | --- |

@@ -946,7 +946,7 @@

(if issued by the governmental authority, please insert a unique identifying number ‘No…’)

### A. **PARTIES**

#### A. **PARTIES**

1.Exporter (name, address and contact details)

@@ -956,7 +956,7 @@

4.Country of final destination

### B. **ITEMS**

#### B. **ITEMS**

1.Items (detailed description of items)

@@ -966,9 +966,7 @@

4.Specification of the end-use location of the items (unless the consignee acts as trader, wholeseller or reseller and is not aware of the end-use location of the items)

### C. **STATEMENT OF FOREIGN CONSIGNEE**

### C.1 **Consignee acts as end-user**

#### C. **STATEMENT OF FOREIGN CONSIGNEE**

Articles 3a(6) and 3c(2) and point (b) of Article 3d(2) of Council Regulation (EU) No 267/2012 require the applicant for an authorisation to submit this end-use statement or an equivalent document containing information on the end-use and end-use location of any supplied item.

@@ -982,8 +980,6 @@

— will only be used for civil end-uses;

— will not be retransferred within Iran without prior information to the exporting State.

### C.2 **Consignee acts as trader, wholeseller or reseller (only to be completed if Section C.1 is not applicable)**

We (I) state that the items described in Section B supplied by the exporter named in Section A 1:

@@ -1011,14 +1007,14 @@

### **CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT**

### **1A** Systems, Equipment and Components

#### **1A** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

| 1A002 | “Composite” structures or laminates, having any of the following: a. Consisting of an organic “matrix” and materials specified in 1C010.c., 1C010.d. or 1C010.e.; or b. Consisting of a metal or carbon “matrix”, and any of the following: 1. Carbon “fibrous or filamentary materials” having all of the following: a. A “specific modulus” exceeding 10,15 × 106 m; and b. A “specific tensile strength” exceeding 17,7 × 104 m; or 2. Materials specified in 1C010.c. *Note 1:* *1A002 does not control composite structures or laminates made from epoxy resin impregnated carbon “fibrous or filamentary materials” for the repair of “civil aircraft” structures or laminates, having all of the following:* *a.* *An area not exceeding 1 m2;* *b.* *A length not exceeding 2,5 m; and* *c.* *A width exceeding 15 mm.* *Note 2:* *1A002 does not control semi-finished items, specially designed for purely civilian applications as follows:* *a.* *Sporting goods;* *b.* *Automotive industry;* *c.* *Machine tool industry;* *d.* *Medical applications.* *Note 3:* *1A002.b.1. does not control semi-finished items containing a maximum of two dimensions of interwoven filaments and specially designed for applications as follows:* *a.* *Metal heat-treatment furnaces for tempering metals;* *b.* *Silicon boule production equipment.* *Note 4:* *1A002 does not control finished items specially designed for a specific application.* | M6A1 | Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A. |

| 1A102 | Resaturated pyrolized carbon-carbon components designed for space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. | M6A2 | Resaturated pyrolised (i.e. carbon-carbon) components having all of the following: a. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or 19.A.1. |

### **1B** Test, Inspection and Production Equipment

#### **1B** Test, Inspection and Production Equipment

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1046,7 +1042,7 @@

| 1B118 | Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following, and specially designed components therefor: a. Two or more mixing/kneading shafts; or b. A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber. | M4B3b | Continuous mixers with provision for mixing under vacuum in the range of zero to 13,326 kPa and with a temperature control capability of the mixing chamber having any of the following: 1. Two or more mixing/kneading shafts; or 2. A single rotating shaft which oscillates and having kneading teeth/pins on the shaft as well as inside the casing of the mixing chamber; |

| 1B119 | Fluid energy mills usable for grinding or milling substances specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls, and specially designed components therefor. | M4B3c | Fluid energy mills usable for grinding or milling substances specified in 4.C |

### **1C** Materials

#### **1C** Materials

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1089,7 +1085,7 @@

| 1C118 | Titanium-stabilised duplex stainless steel (Ti-DSS) having all of the following: a. Having all of the following characteristics: 1. Containing 17,0 – 23,0 weight percent chromium and 4,5 – 7,0 weight percent nickel; 2. Having a titanium content of greater than 0,10 weight percent; and 3. A ferritic-austenitic microstructure (also referred to as a two-phase microstructure) of which at least 10 percent is austenite by volume (according to ASTM E-1181-87 or national equivalents); and b. Having any of the following forms: 1. Ingots or bars having a size of 100 mm or more in each dimension; 2. Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or 3. Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less. | M6C9 | Titanium-stabilized duplex stainless steel (Ti-DSS) usable in the systems specified in 1.A. or 19.A.1. and having all of the following: a. Having all of the following characteristics: 1. Containing 17,0 – 23,0 weight percent chromium and 4,5 – 7,0 weight percent nickel; 2. Having a titanium content of greater than 0,10 weight percent; and 3. A ferritic-austenitic microstructure (also referred to as a two-phase microstructure ) of which at least 10 % is austenite by volume (according to ASTM E-1181-87 or national equivalents); and b. Any of the following forms: 1. Ingots or bars having a size of 100 mm or more in each dimension; 2. Sheets having a width of 600 mm or more and a thickness of 3 mm or less; or 3. Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less. |

| 1C238 | Chlorine trifluoride (ClF3). | M4C4a6 | Compounds composed of fluorine and one or more of other halogens, oxygen or nitrogen; Note: Item 4.C.4.a.6. does not control Nitrogen Trifluoride (NF3) (CAS 7783-54- 2) in a gaseous state as it is not usable for missile applications. |

### **1D** Software

#### **1D** Software

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1098,7 +1094,7 @@

| M6D1 | “Software” specially designed or modified for the operation or maintenance of equipment specified in 6.B.1. | | |

| 1D103 | “Software” specially designed for analysis of reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures. | M17D1 | “Software” specially designed for reduced observables such as radar reflectivity, ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. Note: 17.D.1. includes “software” specially designed for analysis of signature reduction. |

### **1E** Technology

#### **1E** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1128,7 +1124,7 @@

| 2B121 | Positioning tables (equipment capable of precise rotary positioning in any axes), other than those specified in 2B120, having all the following characteristics: a. Two axes or more; and b. A positioning “accuracy” equal to or less (better) than 5 arc second. *Note:* *2B121 does not control rotary tables designed or modified for machine tools or for medical equipment. For controls on machine tool rotary tables see 2B008* | M9B2d | Positioning tables (equipment capable of precise rotary positioning in any axes) having the following characteristics: 1. Two axes or more; and 2. A positioning “accuracy” equal to or less (better) than 5 arc second; |

| 2B122 | Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate slip rings or integrated non-contact devices capable of transferring electrical power, signal information, or both. *Note:* *Centrifuges specified in 2B122 remain controlled whether or not slip rings or integrated non-contact devices are fitted at time of export* | M9B2e | Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate sliprings or integrated non-contact devices capable of transferring electrical power, signal information, or both |

### **2D** Software

#### **2D** Software

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1137,7 +1133,7 @@

| M6D2 | “Software” specially designed or modified for the equipment specified in 6.B.3., 6.B.4. or 6.B.5. | | |

| M15D1 | “Software” specially designed or modified for the “use” of equipment specified in 15.B. usable for testing systems specified in 1.A., 19.A.1. or 19.A.2. or subsystems specified in 2.A. or 20.A. | | |

### **2E** Technology

#### **2E** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1147,7 +1143,7 @@

### **CATEGORY 3 — ELECTRONICS**

### **3A** Systems, Equipment and Components

#### **3A** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1160,13 +1156,13 @@

| b. Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and systems containing those accelerators. *Note:* *3A101.b. above does not specify equipment specially designed for medical purposes.* | M15B5 | Accelerators capable of delivering electromagnetic radiation produced by bremsstrahlung from accelerated electrons of 2 MeV or greater, and equipment containing those accelerators, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A. *Note:* *15.B.5. does not control equipment specially designed for medical purposes.* *Technical Note:* *In Item 15.B. ‘bare table’ means a flat table, or surface, with no fixture or fittings.* | |

| 3A102 | ‘Thermal batteries’ designed or modified for ‘missiles’. *Technical Notes:* *1.* *In 3A102 ‘thermal batteries’ are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery.* *2.* *In 3A102 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.* | M12A6 | Thermal batteries designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2. *Note:* *Item 12.A.6. does not control thermal batteries specially designed for rocket systems or unmanned aerial vehicles that are not capable of a “range” equal to or greater than 300 km.* *Technical Note:* *Thermal batteries are single use batteries that contain a solid non-conducting inorganic salt as the electrolyte. These batteries incorporate a pyrolytic material that, when ignited, melts the electrolyte and activates the battery.* |

### **3D** Software

#### **3D** Software

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

| 3D101 | “Software” specially designed or modified for the “use” of equipment specified in 3A101.b. | M15D1 | “Software” specially designed or modified for the “use” of equipment specified in 3A101.b. |

### **3E** Technology

#### **3E** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1176,7 +1172,7 @@

### **CATEGORY 4 — COMPUTERS**

### **4A** Systems, Equipment and Components

#### **4A** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1187,7 +1183,7 @@

| 4A101 | Analogue computers, “digital computers” or digital differential analysers, other than those specified in 4A001.a.1., which are ruggedized and designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. | M13A1b | Designed as ruggedised or “radiation hardened”. |

| 4A102 | “Hybrid computers” specially designed for modelling, simulation or design integration of space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. *Note:* *This control only applies when the equipment is supplied with “software” specified in 7D103 or 9D103.* | M16A1 | Specially designed hybrid (combined analogue/digital) computers for modelling, simulation or design integration of systems specified in 1.A. or the subsystems specified in 2.A. *Note:* This control only applies when the equipment is supplied with “software” specified in 16.D.1. |

### **4E** Technology

#### **4E** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1197,27 +1193,21 @@

#### ***Part 1 — Telecommunications***

### **5A1** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

| 5A101 | Telemetry and telecontrol equipment, including ground equipment, designed or modified for ‘missiles’. *Technical Note:* *In 5A101 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.* *Note:* *5A101 does not control:* *a.* *Equipment designed or modified for manned aircraft or satellites;* *b.* *Ground based equipment designed or modified for terrestrial or marine applications;* *c.* *Equipment designed for commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight safety) GNSS services;* | M12A4 | Telemetry and telecontrol equipment, including ground equipment, designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2. Notes: 1. 12.A.4. does not control equipment designed or modified for manned aircraft or satellites. 2. 12.A.4. does not control ground based equipment designed or modified for terrestrial or marine applications. 3. 12.A.4. does not control equipment designed for commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight safety) GNSS services. |

### **5D1** Software

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

| 5D101 | “Software” specially designed or modified for the “use” of equipment specified in 5A101. | M12D3 | “Software” specially designed or modified for the “use” of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. |

### **5E1** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

| 5E101 | “Technology” according to the General Technology Note for the “development”, “production” or “use” of equipment specified in 5A101. | M12E1 | “Technology”, in accordance with the General Technology Note, for the “development”, “production” or “use” of equipment or “software” specified in 12.A. or 12.D. |

### **CATEGORY 6 — SENSORS AND LASERS**

### **6A** Systems, Equipment and Components

#### **6A** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1232,14 +1222,14 @@

| 6A108 | Radar systems and tracking systems, other than those specified in entry 6A008, as follows: a. Radar and laser radar systems designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; *Note:* *6A108.a. includes the following:* *a.* *Terrain contour mapping equipment;* *b.* *Imaging sensor equipment;* *c.* *Scene mapping and correlation (both digital and analogue) equipment;* *d.* *Doppler navigation radar equipment.* | M11A1 | Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. *Technical Note:* *Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics.* |

| b. Precision tracking systems, usable for ‘missiles’, as follows: 1. Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity; 2. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities: a. Angular resolution better than 1,5 milliradians; b. Range of 30 km or greater with a range resolution better than 10 m rms; c. Velocity resolution better than 3 m/s. *Technical Note:* *In 6A108.b. ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.* | M12A5 | Precision tracking systems, usable for systems specified in 1.A., 19.A.1. or 19.A.2. as follows: a. Tracking systems which use a code translator installed on the rocket or unmanned aerial vehicle in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of inflight position and velocity; b. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities: 1. Angular resolution better than 1,5 mrad; 2. Range of 30 km or greater with a range resolution better than 10 m rms; and 3. Velocity resolution better than 3 m/s. | |

### **6B** Test, Inspection and Production Equipment

#### **6B** Test, Inspection and Production Equipment

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

| 6B008 | Pulse radar cross-section measurement systems having transmit pulse widths of 100 ns or less, and specially designed components therefor. **N.B.:** **SEE ALSO 6B108.** | M17B1 | Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A |

| 6B108 | Systems, other than those specified in 6B008, specially designed for radar cross section measurement usable for ‘missiles’ and their subsystems. *Technical Note:* *In 6B108 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.* | M17B1 | Systems, specially designed for radar cross section measurement, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A |

### **6D** Software

#### **6D** Software

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1248,7 +1238,7 @@

| M12D3 | “Software” specially designed or modified for the “use” of equipment specified in 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. | | |

| 6D103 | “Software” which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for ‘missiles’. *Technical Note:* *In 6D103 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.* | M12D2 | “Software” which processes post-flight, recorded data, enabling determination of vehicle position throughout its flight path, specially designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2. |

### **6E** Technology

#### **6E** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1258,7 +1248,7 @@

### **CATEGORY 7 — NAVIGATION AND AVIONICS**

### **7A** Systems, Equipment and Components

#### **7A** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1287,7 +1277,7 @@

| c. Flight control servo valves designed or modified for the systems specified in 7A116.a. or 7A116.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz. | M10A3 | Flight control servo valves designed or modified for the systems in 10.A.1. or 10.A.2., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz. *Note:* *Systems, equipment or valves specified in 10.A. may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft.* | |

| 7A117 | “Guidance sets”, usable in “missiles” capable of achieving system accuracy of 3,33 % or less of the range (e.g., a “CEP” of 10 km or less at a range of 300 km). | M2A1d | ‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving system accuracy of 3,33 % or less of the “range” (e.g. a ‘CEP’ of 10 km or less at a “range” of 300 km), except as provided in the Note below 2.A.1. for those designed for missiles with a “range” under 300 km or manned aircraft; |

### **7B** Test, Inspection and Production Equipment

#### **7B** Test, Inspection and Production Equipment

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1303,7 +1293,7 @@

| b. “Production equipment”, and other test, calibration and alignment equipment, other than that specified in 7B001 to 7B003, designed or modified to be used with equipment specified in 7A. | M2B2* | “Production equipment” specially designed for the subsystems specified in 2.A. | |

| M9B1 | “Production equipment”, and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A. *Note:* *Equipment specified in 9.B.1. includes the following:* *a.* *For laser gyro equipment, the following equipment used to characterise mirrors, having the threshold accuracy shown or better:* *1.* *Scatterometer (10 ppm);* *2.* *Reflectometer (50 ppm);* *3.* *Profilometer (5 Angstroms);* *b.* *For other inertial equipment:* *1.* *Inertial Measurement Unit (IMU) Module Tester;* *2.* *IMU Platform Tester;* *3.* *IMU Stable Element Handling Fixture;* *4.* *IMU Platform Balance Fixture;* *5.* *Gyro Tuning Test Station;* *6.* *Gyro Dynamic Balance Station;* *7.* *Gyro Run-In/Motor Test Station;* *8.* *Gyro Evacuation and Filling Station;* *9.* *Centrifuge Fixture for Gyro Bearings;* *10.* *Accelerometer Axis Align Station;* *11.* *Accelerometer Test Station;* *12.* *Fibre Optic Gyro Coil Winding Machines.* | | |

### **7D** Software

#### **7D** Software

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1318,7 +1308,7 @@

| c. Integration “software” designed or modified for the equipment specified in 7A103.c. *Note:* *A common form of integration “software” employs Kalman filtering.* | M9D4 | Integration “software”, designed or modified for the ‘integrated navigation systems’ specified in 9.A.7. *Note:* *A common form of integration “software” employs Kalman filtering.* | |

| 7D103 | “Software” specially designed for modelling or simulation of the “guidance sets” specified in 7A117 or for their design integration with the space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. *Note:* *“Software” specified in 7D103 remains controlled when combined with specially designed hardware specified in 4A102.* | M16D1 | “Software” specially designed for modelling, simulation, or design integration of the systems specified in 1.A. or the subsystems specified in 2.A or 20.A. *Technical Note:* *The modelling includes in particular the aerodynamic and thermodynamic analysis of the systems.* |

### **7E** Technology

#### **7E** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1334,7 +1324,7 @@

### **CATEGORY 9 — AEROSPACE AND PROPULSION**

### **9A** Systems, Equipment and Components

#### **9A** Systems, Equipment and Components

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1399,7 +1389,7 @@

| 9A120 | Liquid propellant tanks, other than those specified in 9A006, specially designed for propellants specified in 1C111 or ‘other liquid propellants’, used in rocket systems capable of delivering at least a 500 kg payload to a range of at least 300 km. | M3A8 | Liquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1. |

| 9A121 | Umbilical and interstage electrical connectors specially designed for “missiles”, space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. *Technical Note:* *Interstage connectors referred to in 9A121 also include electrical connectors installed between the “missile”, space launch vehicle or sounding rocket and their payload.* | M11A5 | Umbilical and interstage electrical connectors specially designed for systems specified in 1.A.1. or 19.A.1. *Technical Note:* *Interstage connectors referred to in 11.A.5. also include electrical connectors installed between systems specified in 1.A.1. or 19.A.1. and their “payload”.* |

### **9B** Test, Inspection and Production Equipment

#### **9B** Test, Inspection and Production Equipment

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1417,7 +1407,7 @@

| M20B1 | “Production facilities” specially designed for the subsystems specified in 20.A. | | |

| 9B117 | Test benches and test stands for solid or liquid propellant rockets or rocket motors, having either of the following characteristics: a. The capacity to handle more than 68 kN of thrust; or b. Capable of simultaneously measuring the three axial thrust components. | M15B3 | Test benches/stands, usable for the systems specified in 1.A., 19.A.1. or 19.A.2. or the subsystems specified in 2.A. or 20.A., which have the capacity to handle solid or liquid propellant rockets, motors or engines having a thrust greater than 68 kN, or which are capable of simultaneously measuring the three axial thrust components. |

### **9C** Materials

#### **9C** Materials

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1425,7 +1415,7 @@

| M3C2 | ‘Insulation’ material in bulk form usable for rocket motor cases in the subsystems specified in 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1. *Technical Note:* *In 3.C.2. ‘insulation’ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps specified in 3.A.3.* | | |

| 9C110 | Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for composite structures, laminates and manufactures specified in 9A110, made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a “specific tensile strength” greater than 7,62 × 104 m and a “specific modulus” greater than 3,18 × 106 m. **N.B.:** **SEE ALSO 1C010 AND 1C210.** *Note:* *The only resin impregnated fibre prepregs specified in entry 9C110 are those using resins with a glass transition temperature (Tg), after cure, exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent.* | M6C1 | Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7,62 × 104 m and a specific modulus greater than 3,18 × 106 m. *Note:* *The only resin impregnated fibre prepregs specified in 6.C.1. are those using resins with a glass transition temperature (Tg), after cure, exceeding 145 °C as determined by ASTM D4065 or national equivalents.* *Technical Notes:* *1.* *In Item 6.C.1. ‘specific tensile strength’ is the ultimate tensile strength in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%.* *2.* *In Item 6.C.1. ‘specific modulus’ is the Young's modulus in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%* |

### **9D** Software

#### **9D** Software

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1443,7 +1433,7 @@

| 9D105 | “Software” which coordinates the function of more than one subsystem, other than that specified in 9D003.e., specially designed or modified for “use” in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104 or ‘missiles’. *Technical Note:* *In 9D105 ‘missile’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.* | M1D2 | “Software” specially designed or modified to coordinate the function of more than one subsystem in systems specified in 1.A. |

| M19D1 | “Software” which coordinates the function of more than one subsystem, specially designed or modified for “use” in the systems specified in 19.A.1. or 19.A.2. | | |

### **9E** Technology

#### **9E** Technology

| The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use items | Missile Technology Control Regime (M.TCR): Equipment, software and technology annex | | |

| --- | --- | --- | --- |

@@ -1456,7 +1446,7 @@

### **Software referred to in Article 10d**

### 1. **Enterprise Resource Planning software, designed specifically for use in nuclear and military industries**

#### 1. **Enterprise Resource Planning software, designed specifically for use in nuclear and military industries**

Explanatory note:Enterprise Resource Planning software is software used for financial accounting, management accounting, human resources, manufacturing, supply chain management, project management, customer relationship management, data services, or access control.

@@ -1830,7 +1820,7 @@

#### 8. Ebrahim MAHMUDZADEH

Former Managing Director of Iran Electronic Industries (see Part B, No 20). Currently director general of the Armed Forces Social Security Organization.

Former Managing Director of Iran Electronic Industries (see Part B, No 20). Director general of the Armed Forces Social Security Organization until September 2020. Iranian Deputy Defense Minister until December 2020.

23.6.2008

—————

@@ -1847,7 +1837,7 @@

#### 13. Anis NACCACHE

Administrator of Barzagani Tejarat Tavanmad Saccal companies; his company has attempted to procure sensitive goods for entities designated under Resolution 1737 (2006).

Former administrator of Barzagani Tejarat Tavanmad Saccal companies; his company has attempted to procure sensitive goods for entities designated under Resolution 1737 (2006).

23.6.2008

#### 14. Brigadier-General Mohammad NADERI

@@ -1856,39 +1846,35 @@

23.6.2008

—————

#### 16. Rear Admiral Mohammad SHAFI'I RUDSARI

Former MODAFL Deputy for Coordination (see Part B, no 29).

#### 16. Rear Admiral Mohammad SHAFI'I RUDSARI (a.k.a. ROODSARI, Mohammad, Hossein, Shafiei; ROODSARI, Mohammad, Shafi’I; ROODSARI, Mohammad, Shafiei; RUDSARI, Mohammad, Hossein, Shafiei; RUDSARI, Mohammad, Shafi’I; RUDSARI, Mohammad, Shafiei)

Former MODAFL Deputy for Coordination (see Part B, n 29).

23.6.2008

17. Abdollah SOLAT SANA

#### Managing Director of the Uranium Conversion Facility (UCF) in Esfahan. This is the facility that produces the feed material (UF6) for the enrichment facilities at Natanz. On 27 August 2006, Solat Sana received a special award from President Ahmadinejad for his role.

17. Abdollah SOLAT SANA (a.k.a. Solatsana

Solat Sanna; Sowlat Senna; Sovlat Thana)

23.4.2007

—————

23. Davoud BABAEI

#### The current head of security for the Ministry Of Defence Armed Forces Logistics' research institute the Organisation of Defensive Innovation and Research (SPND), which is run by UN-designated Mohsen Fakhrizadeh-Mahabadi. The IAEA have identified SPND with their concerns over possible military dimensions to Iran's nuclear programme over which Iran refuses to co-operate. As head of security, Babaei is responsible for preventing the disclosure of information including to the IAEA.

#### The current head of security for the Ministry Of Defence Armed Forces Logistics’ research institute the Organisation of Defensive Innovation and Research (SPND), which was run by UN-designated Mohsen Fakhrizadeh-Mahabadi. The IAEA have identified SPND with their concerns over possible military dimensions to Iran's nuclear programme over which Iran refuses to co-operate. As head of security, Babaei is responsible for preventing the disclosure of information, including to the IAEA.

1.12.2011

—————

25. Sayed Shamsuddin BORBORUDI

(a.k.a. Seyed Shamseddin BORBOROUDI)

DOB: 21/9/1969

Former Deputy Head of UN designated Atomic Energy Organisation of Iran, where he was subordinate to UN designated Feridun Abbasi Davani. Has been involved in the Iranian nuclear programme since at least 2002, including as the former head of procurement and logistics at AMAD, where he was responsible for using front companies such as Kimia Madan to procure equipment and material for Iran’s nuclear weapons programme.

—————

27. Kamran DANESHJOO (a.k.a. DANESHJOU)

#### Former Minister of Science, Research and Technology. He has provided support for Iran's proliferation-sensitive nuclear activities.

1.12.2011

—————

#### 27. Kamran DANESHJOO (a.k.a. DANESHJOU)

Former Minister of Science, Research and Technology. He has provided support for Iran's proliferation-sensitive nuclear activities.

1.12.2011

—————

29. Milad JAFARI

date of birth 20.9.74

An Iranian national supplying goods, mostly metals, to UN designated SHIG front companies. Delivered goods to SHIG between January and November 2010. Payments for some of the goods were made at the central branch of EU-designated Export Development Bank of Iran (EDBI) in Tehran after November 2010.

29. Milad JAFARI (Milad JAFERI)

DOB: 20.9.1974

1.12.2011

—————

@@ -1909,28 +1895,28 @@

1.12.2011

—————

## 37. Mohammad Sadegh NASERI

### Head of the Physics Research Institute (formerly known as the Institute of Applied Physics).

37. Mohammad Sadegh NASERI

## Head of the Physics Research Institute (formerly known as the Institute of Applied Physics).

1.12.2011

—————

40. Hamid SOLTANI

### 40. Hamid SOLTANI

Managing Director of the EU-designated Management Company for Nuclear Power Plant Construction (MASNA)

1.12.2011

—————

## 42. Javad AL YASIN

### Head of the Research Centre for Explosion and Impact, also known as METFAZ

42. Javad AL YASIN

## Head of the Research Centre for Explosion and Impact, also known as METFAZ

1.12.2011

—————

B. *Entities*

Name

### Name

Identifying information

Reasons

Date of listing

@@ -1939,9 +1925,10 @@

Langare Street,Nobonyad Square,Tehran, Iran

AIO oversees Iran's production of missiles, including Shahid Hemmat Industrial Group, Shahid Bagheri Industrial Group and Fajr Industrial Group, which were all designated under UNSCR 1737 (2006). The head of AIO and two other senior officials were also designated under UNSCR 1737 (2006)

23.4.2007

2. Armed Forces Geographical Organisation

Assessed to provide geospatial data for the Ballistic Missile programme

2. Armed Forces Geographical Organisation

A subsidiary of MODAFL assessed to provide geospatial data for the Ballistic Missile programme.

23.6.2008

—————

@@ -2034,19 +2021,26 @@

20. Iran Electronics Industries

(including all branches) and subsidiaries:

P. O. Box 18575-365, Tehran, Iran

Wholly-owned subsidiary of MODAFL (and therefore a sister-organisation to AIO, AvIO and DIO). Its role is to manufacture electronic components for Iranian weapons systems.

23.6.2008

(a) Isfahan Optics

P.O. Box 81465-313 Kaveh Ave. Isfahan - Iran

P.O. Box 81465-117, Isfahan, Iran

Owned, controlled by, or acts on behalf of Iran Electronics Industries

26.7.2010

(b) Iran Communications Industries (ICI)

PO Box 19295-4731, Pasdaran Avenue, Tehran, Iran; Alternative address: PO Box 19575-131, 34 Apadana Avenue, Tehran, Iran; Alternative address: Shahid Langary Street, Nobonyad Square Ave, Pasdaran, Tehran

(b) Iran Communications Industries (ICI)

(a.k.a. Sanaye Mokhaberat Iran;

Iran Communication Industries;

Iran Communications Industries Group;

Iran Communications Industries Co.)

Iran Communications Industries, a subsidiary of Iran Electronics Industries (listed by the EU), produces various items including communication systems, avionics, optics and electro-optics devices, micro-electronics, information technology, test and measurement, telecommunication security, electronic warfare, radar tube manufacture and refurbishment, and missile launchers.

26.7.2010

21. ██████

██████

@@ -2070,10 +2064,13 @@

—————

28. Mechanic Industries Group

(a.k.a.: Mechanic Industries Organisation; Mechanical Industries Complex; Mechanical Industries Group; Sanaye

Mechanic)

Took part in the production of components for the ballistics programme.

23.6.2008

29. Ministry Of Defense And Support For Armed Forces Logistics (a.k.a. Ministry Of Defense For Armed Forces Logistics; a.k.a. MODAFL; a.k.a. MODSAF)

Located on the west side of Dabestan Street, Abbas Abad District, Tehran, Iran

Responsible for Iran's defence research, development and manufacturing programmes, including support to missile and nuclear programmes.

23.06.2008

@@ -2102,20 +2099,23 @@

—————

37. Schiller Novin

Gheytariyeh Avenue - no 153 - 3rd Floor - PO BOX 17665/153 6 19389 Teheran

(a.k.a.: Schiler Novin Co.; Schiller Novin Co.; Shiller Novin)

Gheytariyeh Avenue - no 153 - 3rd Floor - PO BOX 17665/153 6 19389 Tehran

Acting on behalf of Defense Industries Organisation (DIO).

26.7.2010

38. Shahid Ahmad Kazemi Industrial Group

SAKIG develops and produces surface-to-air missiles systems for Iran's military. It maintains military, missile, and air defense projects and procures goods from Russia, Belarus, and North Korea.

26.7.2010

39. Shakhese Behbud Sanat

38. Shahid Ahmad Kazemi Industrial Group (SAKIG)

Entity subordinate to Iran’s Aerospace Industries Organisation (AIO). SAKIG develops and produces surface-to-air missiles systems for Iran's military. It maintains military, missile, and air defense projects and procures goods from Russia, Belarus, and North Korea.

26.7.2010

39. Shakhese Behbud Sanat

Involved in the production of equipment and parts for the nuclear fuel cycle.

26.7.2010

40. State Purchasing Organisation (SPO)

The SPO appears to facilitate the import of whole weapons. It appears to be a subsidiary of MODAFL

40. State Purchasing Organisation (SPO, a.k.a. State Purchasing Office; State Purchasing Organization)

The SPO appears to facilitate the import of whole weapons. It appears to be a subsidiary of MODAFL.

23.6.2008

41. Technology Cooperation Office (TCO) of the Iranian President's Office (a.k.a.

@@ -2183,10 +2183,10 @@

—————

52. Raad Iran (a.k.a Raad Automation Company)

Unit 1, No 35, Bouali Sina Sharghi, Chehel Sotoun Street, Fatemi Square, Tehran

A company involved in procurement of inverters for Iran's proscribed enrichment programme. RaadIran was established to produce and design controlling systems and provides the sale and installation of inverters and programmable Logic Controllers.

23.05.2011

52. Raad Iran (a.k.a. Raad Automation Company; Middle East Raad Automation; RAAD Automation Co.; Raad Iran Automation Co.; RAADIRAN, Middle East RAAD Automation Co.; Automasion RAAD Khavar Mianeh; Automation Raad Khavar Mianeh Nabbet Co)

Unit 1, No 35, Bouali Sina Sharghi, Chehel Sotoun Street, Fatemi Square, Tehran

A company involved in procurement of inverters for Iran's proscribed enrichment programme. Raad Iran was established to produce and design controlling systems and provides the sale and installation of inverters and programmable Logic Controllers.

23.5.2011

—————

54. Sun Middle East FZ Company

@@ -2300,9 +2300,10 @@

██████

86. Karanir (a.k.a. Moaser, a.k.a. Tajhiz Sanat)

1139/1 Unit 104 Gol Building, Gol Alley, North Side of Sae, Vali Asr Avenue. PO Box 19395-6439, Tehran.

Involved in purchasing equipment and materials which have direct applications in the Iranian nuclear programme.

86. Karanir (a.k.a Karanir Sanat, Moaser; Tajhiz Sanat)

1139/1 Unit 104 Gol Building, Gol Alley, North Side of Sae, Vali Asr Avenue. PO Box 19395-6439, Tehran

Involved in purchasing equipment and materials, which have direct applications in the Iranian nuclear programme.

1.12.2011

87. Khala Afarin Pars (a.k.a. PISHRO KHALA AFARIN COMPANY)

@@ -2341,8 +2342,8 @@

Engineering firm involved in supporting a range of large scale industrial projects including Iran's uranium enrichment programme, including undeclared work at the uranium enrichment site at Qom/Fordow.

1.12.2011

95. Samen Industries

2nd km of Khalaj Road End of Seyyedi St., P.O.Box 91735-549, 91735 Mashhad, Iran, Tel.: +98 511 3853008, +98 511 3870225

95. Samen Industries (a.k.a. Khorasan Metallurgy Industries)

2nd km of Khalaj Road End of Seyyedi St., P.O.Box 91735-549, 91735 Mashhad, Iran, Tel.: +98 511 3853008, +98 511 3870225

Shell name for UN-designated Khorasan Metallurgy Industries, subsidiary of Ammunition Industries Group (AMIG).

1.12.2011

—————

@@ -2355,11 +2356,15 @@

Company for Construction and Commissioning of Nuclear Power Plants. Controlled by the UN designated Novin Energy Company.

1.12.2011

99. TABA (Iran Cutting Tools Manufacturing company - Taba Towlid Abzar Boreshi Iran)

12 Ferdowsi, Avenue Sakhaee, avenue 30 Tir (sud), nr 66 – Tehran

Owned or controlled by EU-sanctioned TESA, Involved in manufacturing equipment and materials which have direct applications in the Iranian nuclear programme.

99. TABA (Iran Cutting Tools Manufacturing company - Taba Towlid Abzar Boreshi Iran;

a.k.a. Iran Centrifuge Technology Co.; Iran's Centrifuge Technology Company; Sherkate Technology Centrifuge

Iran, TESA, TSA)

12 Ferdowsi, Avenue Sakhaee, avenue 30 Tir (sud), nr 66 – Tehran

Owned or controlled by EU-sanctioned TESA, Involved in manufacturing equipment and materials, which have direct applications in the Iranian nuclear programme.

1.12.2011

100. Test Tafsir

No 11, Tawhid 6 Street, Moj Street, Darya Blvd, Shahrak Gharb, Tehran, Iran.

Company produces and has supplied UF6 specific containers to the uranium enrichment sites at Natanz and Qom/Fordow.

1.12.2011

@@ -2441,15 +2446,15 @@

153. Organisation of Defensive Innovation and Research (SPND)

The Organisation of Defensive Innovation and Research (SPND) directly supports Iran's proliferation sensitive nuclear activities. The IAEA has identified SPND with their concerns over possible military dimensions (PMD) to Iran's nuclear programme. SPND is run by UN-designated Mohsen Fakhrizadeh-Mahabadi and is part of the Ministry of Defence For Armed Forces Logistics (MODAFL) designated by the EU.

The Organisation of Defensive Innovation and Research (SPND) directly supports Iran's proliferation sensitive nuclear activities. The IAEA has identified SPND with their concerns over possible military dimensions (PMD) to Iran's nuclear programme. SPND was run by UN-designated Mohsen Fakhrizadeh-Mahabadi and is part of the Ministry of Defence For Armed Forces Logistics (MODAFL) designated by the EU.

22.12.2012

—————

161. Sharif University of Technology

Last address known: Azadi Ave/Street, PO Box 11365-11155, Tehran, Iran, Tel. +98 21 66 161 Email: info@sharif.ir

Sharif University of Technology (SUT) has a number of cooperation agreements with Iranian Government organisations which are designated by the UN and/or the EU and which operate in military or military-related fields, particularly in the field of ballistic missile production and procurement. This includes: an agreement with the EU-designated Aerospace Industries Organisation for, inter alia, the production of satellites; cooperating with the Iranian Ministry of Defence and the Iranian Revolutionary Guards Corps (IRGC) on smart boat competitions; a broader agreement with the IRGC Air Force which covers developing and strengthening the University’s relations, organisational and strategic cooperation; SUT is part of a 6-university agreement which supports the Government of Iran through defence-related research.

Last address known: Azadi Ave/Street, PO Box 11365-11155, Tehran, Iran, Tel. +98 21 66 161 Email: info@sharif.ir

Taken together, these show a significant record of engagement with the Government of Iran in military or military-related fields that constitutes support to the Government of Iran.

8.11.2014

@@ -2496,7 +2501,7 @@

2. Rear Admiral Ali FADAVI

Commander of IRGC Navy

Deputy Chief of the Islamic Revolutionary Guard Corps (IRGC). Former Commander of IRGC Navy.

26.7.2010

3. Parviz FATAH

@@ -2514,9 +2519,10 @@

6. IRGC Mohammad Ali JAFARI

Former Commander of the IRGC.

Former Commander of the IRGC. Currently head of the Hazrat Baqiatollah al-Azam Cultural and Social Headquarters.

23.6.2008

7. IRGC Brigadier-General Mostafa Mohammad NAJJAR

Former Minister for the Interior and former Minister of MODAFL, responsible for all military programmes, including ballistic missiles programmes. Currently, senior advisor to the Chief of General Staff of the Armed Forces.

23.6.2008

@@ -2621,6 +2627,8 @@

23.1.2012

12. Etemad Amin Invest Co Mobin

(a.k.a.: Etemad Amin Investment Company Mobin; Etemad-e Mobin, Etemad Amin Invest Company Mobin; Etemad Mobin Co.;

Etemad Mobin Trust Co.; Etemade Mobin Company; Mobin Trust Consortium; Etemad-e Mobin Consortium)

Pasadaran Av. Tehran, Iran

A company owned or controlled by IRGC that contributes to financing the strategic interests of the regime.

26.7.2010

2020-11-14

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2020-06-20

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2019-07-09

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2019-05-29

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2018-06-07

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2017-06-25

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2017-01-18

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2016-10-23

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2016-08-17

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2016-04-21

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2016-01-23

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2016-01-16

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2015-12-01

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2015-08-02

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2015-06-27

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2015-04-08

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2015-02-15

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2014-11-08

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2014-04-23

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2014-01-20

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2013-12-19

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2013-10-12

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2013-06-08

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2012-12-23

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2012-11-16

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2012-10-16

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2012-08-03

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning restric

View changes Text at this date

2012-04-24

Council Regulation (EU) No 267/2012 of 23 March 2012 concerning rest

original version Text at this date