Item No.

Name <*>

Commodity Nomenclature of Foreign Economic Activity code <*>

Section 1

Category 1. Special materials and related equipment and equipment

1.1.

Systems, equipment and components

1.1.1.

The components made of the fluorinated connections:

1.1.1.1.

Consolidations, laying, the sealing materials or fuel tanks which are specially developed for use in flying or space devices and made of the materials containing more than 50 percent (on weight) any material determined in Item 1.3.9.1 or 1.3.9.2;

3919 90 000 0;

3926;

8807

1.1.2.

Designs from the following composition materials of volume or layered structure:

1.1.2.1.

Consisting of any following materials:

3926 90 920 0;

3926 90 970

a) the organic matrix and fibrous or threadlike materials determined in Item 1.3.10.3 or 1.3.10.4; or

b) the prepreg and preforms determined in Item 1.3.10.5;

1.1.2.2.

Consisting of metal or carbon matrix and any of the following:

1.1.2.2.1.

The carbon fibrous or carbon threadlike materials having all following characteristics:

3801;

3926 90 920 0;

3926 90 970;

6903 10 000 0

a) the specific module of elasticity exceeding 10, 15 x 106 m; and

b) the specific durability in case of stretching exceeding 17, 7 x 104 m; or

Note.

Item 1.1.2.2.1 is not applied:

a) to the semi-ready designs having maximum two-dimensional interlacing of threads and which are specially developed for the following use:

1) in furnaces for heat treatment of metals;

2) in the equipment for production silicon buly;

b) to mechanically split, crushed or cut off carbon fibrous or threadlike materials 25 mm long or less

1.1.2.2.2.

The materials determined in Item 1.3.10.3

Notes:

1. Item 1.1.2 is not applied to the elements of designs from composition materials of volume or layered structure made of the carbon fibrous or threadlike materials impregnated with epoxy, to repair of civil aircraft, having all following:

a) the area which is not exceeding 1 sq.m;

b) length which is not exceeding m 2,5; and

c) width more than 15 mm.

2. Item 1.1.2 is not applied to partially made designs specially developed for only the following civil use:

a) in sports goods;

b) in automotive industry;

c) in machine-tool industry;

d) in the medical purposes.

3. Item 1.1.2 is not applied to completely made goods (designs) which are specially developed for specific use

Special note.

Concerning designs from the composition materials specified in Items 1.1.2 - 1.1.2.2.2, cm also Item 1.1.1 of Section 2 and Item 1.1.1 of Section 3

1.1.3.

Products from not fusible aromatic polyamides (aramids) in the form of film, leaf, the tapes or strips having any of the following characteristics:

3919 90 000 0;

3920 99 900 0

a) thickness of more 0,254 of mm; or

b) covering or lamination by carbon, graphite, metals or magnetic substances

Note.

Item 1.1.3 is not applied to the products covered or laminated by copper and developed for production of electronic printed circuit boards

Special note.

For fusible aromatic polyamides (aramids) in any kind see Item 1.3.8.1.3

1.1.4.

The protective equipment, the equipment of detection systems and components which are not specially developed for military application:

1.1.4.1.

The gas masks filtering boxes of gas masks and the equipment for their disinfecting developed or modified for protection against any of the below-stated striking factors and also the components which are specially developed for them:

8421 39 200 8;

9020 00 000 0;

9033 00 000 0

a) bacteriological (biological) agents;

b) radioactive materials;

c) the chemicals used in chemical weapon; or

d) the chemical means for fight against mass riots including:

-brombenzenolatsetonitril (brombenzylcyanide) (CA) (CAS 5798-79-8);

[(2 chlorophenyl) methylene] pro-pan-dinitrile (au chlorbenzylpropane dinitrile) (CS) (CAS 2698-41-1);

2-chlorine-1-feniletanol, fenilatsetit chloride (-chloracetophenone) (CN) (CAS 532-27-4);

dibenz-(b, f) - 1, 4-oksazepin (CR) (CAS 257-07-8);

10-chlorine-5,10-digidrofenarsazin, (chloride фенарсазин), (adamsite) (DM) (CAS 578-94-9);

N-nonanoilmorfolin (MPA) (CAS 5299-64-9)

Note.

Item 1.1.4.1 includes the gas masks with forced air supply developed or modified for protection against the striking factors listed in Item 1.1.4.1

Technical note.

For the purposes of Item 1.1.4.1:

a) gas masks are also called full-front masks;

b) the filtering boxes of gas masks also include the filtering cartridges;

1.1.4.2.

Protective suits, gloves and footwear, specially developed or modified for protection against any of the below-stated striking factors:

3926 20 000 0;

4015 12 000 9;

4015 19 000 0;

4015 90 000 0;

6204 23;

6210 40 000 0;

6210 50 000 0;

6216 00 000 0;

6401 92;

6401 99 000 0;

6402 91;

6402 99 100 0;

6402 99 930 0;

6404 19 900 0

a) bacteriological (biological) agents;

b) radioactive materials; or

c) the chemicals used in chemical weapon;

1.1.4.3.

Systems, specially developed or modified for detection or recognition of any of the below-stated striking factors, and also the components which are specially developed for them:

9027 10 100 0;

9027 10 900 0;

9027 81 000 0;

9027 90 800 0;

9030 10 000 0;

9030 89 300 0;

9030 89 900 9;

9030 90 850 0;

a) bacteriological (biological) agents;

b) radioactive materials; or

c) the chemicals used in chemical weapon

1.1.4.4.

The electronic equipment and its components developed for automatic detection or recognition of availability of traces of the explosives (E) with use of methods of their detection (for example, superficial acoustic wave, spectrometry of mobile ions, including with differential mobility, mass spectrometry)

9027 10 100 0;

9027 30 000 0;

9027 81 000 0;

9027 90 800 0;

9030 89 300 0

Technical note.

Detection of traces is understood as detection of less million part of evaporation or 1 mg of solid substance or liquid

Note.

Item 1.1.4.4 is not applied:

a) to the equipment which is specially developed for laboratory use;

b) to throughput portals of safety for non-contact control

Note.

Item 1.1.4 is not applied:

a) to personal radiation dosimeters;

b) to the equipment or systems applied in occupational safety standards system, structurally or functionally limited by protection against risk factors for the purpose of safety in civil area, for example:

in mining;

during the work in pits;

in agricultural industry;

in pharmaceutical industry;

in the medical industry;

in veterinary science;

during the works on environmental protection;

in case of collection and waste recycling;

in the food industry

Technical notes:

1. Item 1.1.4 includes equipment, systems and their components which were certified, or their working capacity concerning detection or protection against radioactive materials, bacteriological (biological) agents, the chemicals used in chemical weapon, the imitating products (substitutes) or chemical means for fight against mass riots was confirmed with the testing which are carried out according to national standards, or otherwise even if such systems, the equipment or their components are used in civil areas, such as mining, works in pits, agricultural industry, the pharmaceutical and medical industry, veterinary science, environmental protection, collection and waste recycling or the food industry.

2. The imitating products (substitutes) - substances or materials which are used instead of toxic substances (chemical or biological) for training, research, approbation or assessment.

3. For the purposes of Item 1.1.4 radioactive materials are the radioisotopes allocated or modified for harming the person or animal, removal from system of the equipment, causing damage to harvest or the environment

1.1.5.

Bullet-proof vests and components for them:

1.1.5.1.

The bullet-proof vests made not according to military standards or specifications or unequal by it according to characteristics, and components which are specially developed for them, including (including) flexible protective elements;

6211 43 900 0

6914 90 000 0

1.1.5.2.

The tough plates for bullet-proof vests providing class of ballistic protection, equal IIIA or less according to the standard of National institute of justice of the USA of NIJ 0101.06 (July, 2008) or equivalent standards

3926 90 920 0;

6914 90 000 0;

7326 19 100 0;

7326 19 900 9;

7326 90 940 9;

7326 90 980 7

Notes:

1. Item 1.1.5 is not applied to bullet-proof vests which are exported by the user for own individual protection.

2. Item 1.1.5 is not applied to the bullet-proof vests developed for ensuring only frontal protection both against splinters and from explosion of not military destructive devices.

3. Item 1.1.5 is not applied to the bullet-proof vests developed for protection only against the kolyushche-cutting or blunt objects

Special note.

For the threadlike and fibrous materials used in production of bullet-proof vests see Item 1.3.10

1.1.6.

The equipment, specially developed or modified for neutralization of improvised explosive devices, stated below, and also specially developed components and accessories to it:

1.1.6.1.

Remotely-controlled vehicles;

1.1.6.2

Podryvateli (destroyers)

8424 30;

8424 89 000 9;

8479 89 970 7

Technical note.

For the purposes of Item 1.1.6.2 podryvatel (destroyers) are the devices which are specially developed for prevention of operation of the destructive device by impact by liquid, firm or loose shell

Note.

Item 1.1.6 is not applied to the equipment which equips directly the operator

1.1.7.

The equipment and devices which are specially developed for initiation of the charges and devices containing energy materials, electricity impact:

1.1.7.1.

The starting devices (ignition systems) developed for actuating of the detonators of explosive determined in Item 1.1.7.2;

8543 70 800 0;

9306 90 900 0

1.1.7.2.

Explosive electrodetonators, such, as:

1.1.7.2.1.

Detonators with the exploding bridge (EB) (spark detonators);

3603 60 000 0

1.1.7.2.2.

Detonators with the blowing-up crossing point from wire (current detonators);

3603 60 000 0

1.1.7.2.3.

Detonators with the drummer (punch) (detonators of shock action);

3603 30 000 0

1.1.7.2.4.

Initiators with the blowing-up foil

3603 60 000 0

Technical notes:

1. The concept "detonator" also includes the concept "initiator" or "zazhigatel".

2. For the purposes of Item 1.1.7.2 in all detonators described in it the small electric conductor (the bridge, crossing point from wire or foil) which evaporates with the explosion caused by passing through it short silnotochny electric impulse is used. In detonators of unaccented action the blowing-up conductor initiates chemical detonation in the brisant explosive contacting to it, such as TEN (PETN) - tetranitropentaerythritol. In detonators of shock action (like Slepper) the evaporation of the electric conductor caused by explosion puts in action of baizes or punch which influences explosive and initiates chemical detonation. In some designs the drummer is set in motion by force of magnetic field. The term "the initiator with the blowing-up foil" can belong both to VM, and to detonator of shock action (like Slepper)

1.1.8.

Charges, devices and components:

1.1.8.1.

The cumulative charges having everything following characteristics:

3604 90 000 0

a) quantity net VV (QNV) more than 90 g; and

b) the external diameter of cover equal or is more than 75 mm;

1.1.8.2.

The cumulative linear charges for cutting having everything following characteristics, and components which are specially developed for them:

3604 90 000 0

a) VV charge more than 40 g/m; and

b) width equal or it is more than 10 mm;

1.1.8.3.

The cord detonating with internal charge of VV more than 64 g/m;

3603 20 000

1.1.8.4.

Cutting torches, excellent from determined in Item 1.1.8. 2, and other detachable means having KNV more 3,5 of kg

3604 90 000 0

Technical note.

Cumulative charges - the devices concentrating action of VV in the course of its explosion

Note.

To the charges and devices determined in Item 1.1. 8, only those charges which contain VV listed in the table to this Item, and their mix belong

Item No.

Name of explosives

1.

Aminodinitrobenzofuroksan (ADNBF; 7-amino-4,6-dinitropetrolfuradhan-1-oxide) (CAS 97096-78-1)

2.

Cis-bis (5-tetranitrazolato) tetraamine-cobalt (III) perchlorate (BNCP) (CAS 117412-28-9)

3.

Diaminodinitrobenzofuroksan (CL-14; 5,7-диамино-4,6-динитробензофуразан-1-оксид) (CAS 117907-74-1)

4.

Geksanitrogeksaazaizovyurtsitan (CL-20; HNIW) (CAS 135285-90-4);

clathrates (connections/inclusions) of the substance CL-20

5.

2-(5-tsianotetrazolato) pentaamine-cobalt (III) perchlorate (CP) (CAS 70247-32-4)

6.

1, ((((((((((((((((((((((((((((((((DADE; FOX7) (CAS 145250-81-3)

7.

Diaminotrinitrobenzol (DATB) (CAS 1630-08-6)

8.

1, (((((((((((((((((((((((((((((DDFP)

9.

2, (((((((((((((((((((((((((((((((((((((((((DDPO; PZO) (CAS 194486-77-6)

10.

3,3" - diamino-2,2", 4,4", 6,6" - hexanitrobiphenyl (DIPAM; дипикрамид) (CAS 17215-44-0)

11.

Dinitroglikolyuril (DNGU; DINGU) (CAS 55510-04-8)

12.

Furadhans:

a) diaminoazoxyfuradhan (DAAOF);

b) diaminoazofuradhan (DAAzF) (CAS 78644-90-3)

13.

Octogene (HMX) and its derivatives:

a) циклотетраметилентетранитрамин (HMX; octogene; октагидро-1,3,5,7-тетранитро-1,3,5,7-тетразин; 1,3,5,7-тетранитро-1,3,5,7-тетразациклооктан) (CAS 2691-41-0);

b) diftoraminirovanny analogs of octogene;

c) 2,4,6,8-тетранитро-2,4,6,8-тетраазабицикло [3,3,0] - oktanon-3 (tetranitrosemiglikourit; keto-bicyclic octogene; K-55) (CAS 130256-72-3)

14.

hexanitroadamantan (HNAD) (CAS 143850-71-9)

15.

Hexanitrostilbene (HNS) (CAS 20062-22-0)

16.

Imidazoles:

a) octahydro-2,5-bis (nitroimino) имидазо [4,5-d] imidazole (BNNII);

b) 2,4 - dinitroimidazole (DNI) (CAS 5213-49-0);

c) 1-fluorine-2,4-dinitroimidazole (FDIA);

d) N-(2-нитротриазоло) - 2,4 - dinitroimidazole (NTDNIA);

e) 1-picryl-2, 4, 5-trinitroimidazol (PTIA)

17.

1-(2-nitrotriazolo) - 2-dinitrometilengidrazin (NTNMH)

18.

3-nitro-1, 2,4 - triazole - 5 - it (NTO; ONTA) (CAS 932-64-9)

19.

Polinitrokubana with number of nitrogroups more than four

20.

2,6 - bis (pikrilamino) - 3,5 - dinitropyridine (PYX) (CAS 38082-89-2)

21.

Hexogen (RDH) and its derivatives:

a) cyclotrimethylenetrinitramine (hexogen; RDX; trimethylene trinitramine; T4; geksagidro-1, 3, 5-trinitro-1, 3,5 - triazine; 1,3, 5-trinitro-1, 3,5 - triazacyclohexane) (CAS 121-82-4);

b) keto-hexogen (Keto-RDX; K-6; 2,4, 6-trinitro-2, 4,6 - triazacyclohexanone) (CAS 115029-35-1)

22.

Triaminoguanidinnitrat (TAGN) (CAS 4000-16-2)

23.

Triaminotrinitrobenzene (TATB) (CAS 3058-38-6)

24.

3,3,7,7 - tetrabis (дифторамин) octahydro-1,5-dinitro-1,5-diazocine (TEDDZ)

25.

Tetrazoles:

a) nitrotriazolaminotetrazole (NTAT);

b) 1-N-(2-нитротриазоло) - 4 nitrotetrazole (NTNT)

26.

Trinitrofenilmetilnitramin (tetryl) (CAS 479-45-8)

27.

1,4,5,8-тетранитро-1,4,5,8-тетраазадекалин (TNAD) (CAS 135877-16-6)

28.

1,3, 3-trinitroazetidin (TNAZ) (CAS 97645-24-4)

29.

Tetranitroglikolyuril (TNGU; SORGUYL) (CAS 55510-03-7)

30.

1,4,5, 8-tetranitropiridazino [4,5-d] pyridazinum (TNP) (CAS 229176-04-9)

31.

Triazines:

a) 2-oxy-4,6-dinitroamino-S-triazine (DNAM) (CAS 19899-80-0);

b) 2-нитроимино-5-нитро-гексагидро-1,3,5-триазин (NNHT) (CAS 130400-13-4)

32.

Triazoles:

a) 5-azido-2-nitrotriazole;

b) 2,4 - 4-amino-3,5-digidrazino-1, triazole dinitramide (ADHTDN) (CAS 1614-08-0);

c) 1-amino-3,5-dinitro-1, 2,4 - triazole (ADNT);

d) encore (dinitrotriazole) amine) (BDNTA);

e) 3,3" - 2,4 - dinitro-5,5-bi-1, triazole (DBT) (CAS 30003-46-4);

e) динитробистриазол (DNBT) (CAS 70890-46-9);

g) 1-N-(2-нитротриазоло) 3,5 - dinitrotriazole (NTDNT);

h) 1-picryl-3,5-dinitrotriazole (PDNT);

i) tetranitropetroltriazoloazimido-benzene (TACOT) (CAS 25243-36-1)

33.

The VV which are not named in this list, having at the maximum density detonation speed more than 8700 m/s or pressure of detonation more than 34 GPA (340 Kbar)

34.

Nitrocellulose with content of nitrogen of more 12,5 of percent (CAS 9004-70-0)

35.

Nitroglycol (CAS 628-96-6)

36.

Tetranitropentaeritrit (pentaerythritoltetra nitrate; пентаэритритолтетранитрат; TEN; PETN) (CAS 78-11-5)

37.

Pikrilkhlorid (CAS 88-88-0)

38.

2,4,6 - trinitrotoluene (TNT) (CAS 118-96-7)

39.

Nitroglycerine (NG) (CAS 55-63-0)

40.

Triatsetontriperoksid (TATP) (CAS 17088-37-8)

41.

Guanidine nitrate (CAS 506-93-4)

42.

Nitroguanidine (NQ) (CAS 556-88-7)

43.

2, ((((((((((((((((DNAN) (CAS 119-27-7)

44.

4,10-динитро-2,6,8,12-тетраокса-4,10-диазаизовюрцитан (TEX)

45.

dinitramide guanyl-urea (GUDN) FOX-12 (CAS 217464-38-5)

46.

Tetrazines:

a) encore (2,2,2 - trinitrate) - 3,6 - diaminotetrazine (BTAT)

b) 3,6-диамино-1,2,4,5-тетразина-1,4-диоксид (LAX-112)

47.

The energy ionic materials melting at temperatures from 343 K (70 °C) to 373 K (100 °C) and having detonation speed more than 6800 m/s or pressure of blast wave more than 18 GPA (180 Kbar)

48.

Encore (2,2, 2-trinitroetit) нитрамин (BTNEN) (CAS 19836-28-3)

49.

5,6-(3", 4" - furadhan) - 1,2,3, 4-tetrazine-1,3-dioxide (FTDO)

50.

Etilendinitramin (EDNA) (CAS 505-71-5)

51.

Digidroksilammoniya 5,5" - bistetrazol-1,1" - thiolate (TKX-50)

Item No.

Name <*>

Commodity Nomenclature of Foreign Economic Activity code <*>

1.2.

Test, control and production equipment

1.2.1.

The equipment which is stated below for production or control of designs from the composition materials of volume or layered structure determined in Item 1.1. 2, or the fibrous or threadlike materials determined in Item 1.3. 10, and also the components and auxiliary devices which are specially developed for it:

1.2.1.1.

The machines for winding of fibers which are specially developed for production of designs from composition materials of volume or layered structure from fibrous or threadlike materials in which the movements connected with positioning, impregnation and winding of fibers are coordinated and programmed on three or more axes of the main servo positioning;

8445 40 000;

8445 90 000 1

1.2.1.2.

Machines for the calculation of tape in which the movements connected with positioning and stacking of tape are coordinated and programmed on five or more axes of the main servo positioning and which are specially developed for production of elements of designs of aircraft or rockets from composition materials

8445 40 000;

8445 90 000 1

Technical note.

For the purposes of machine Item 1.2.1.2 for the calculation of tape have capability of the calculation of one threadlike tape or more than width from more 25,4 of mm to mm 304,8 inclusive, and also tapes and renewals of separate transactions during process of the calculation are sharp;

1.2.1.3.

Multicoordinate weaver's machines or machines for weaving, including devices and devices, specially developed or modified for weaving, weaving or interlacing of fibers for designs from composition materials of volume structure

8446 30 000 0;

8447 90 000

Technical note.

For the purposes of Item 1.2.1.3 weaving includes knitting;

1.2.1.4.

The equipment, specially developed or adapted for production of the reinforcing fibers:

1.2.1.4.1.

The equipment for transformation of polymeric fibers (such, as polyacrylonitrile, viscose, peak or polikarbosilanovy) in carbon or karbidkremniyevy fibers, including the special equipment for tension of fibers when heating;

8456 40 000 0;

8456 90 000 0;

8515 80 900 0

1.2.1.4.2.

The equipment for chemical sedimentation of elements or connections from steam phase on heated threadlike substrate for the purpose of production of karbidkremniyevy fibers;

8419 89 989 0

1.2.1.4.3.

The equipment for receipt of refractory ceramic fibers (for example, from aluminum oxide) on wet method;

8445 90 000 9

1.2.1.4.4

The equipment for transformation by heat treatment of fibers of aluminum-bearing precursors to aluminum oxide fibers;

8514 11 000 0;

8514 19 900 0;

8514 20 100 0;

8514 20 800 0;

8514 31 000 0;

8514 32 000 0;

8514 39 000 0;

8514 40 000 0

1.2.1.5.

The equipment for production of the prepreg determined in Item 1.3.10. 5, by method of hot melting;

8451 80 800 9;

8477 59 100 0;

8477 59 800 0

1.2.1.6.

The equipment for nondestructive control which is specially developed for composition materials such, as:

1.2.1.6.1.

Systems of x-ray tomography for three-dimensional detection of defects;

9022 12 000 0;

9022 19 000 0;

9022 29 000 0

1.2.1.6.2.

Installations of ultrasonic defectoscopy with numerical control in which movements for positioning of transmitters or receivers are at the same time coordinated and programmed on four or more axes to trace three-dimensional contours of the inspected object;

9031 80 380 0

1.2.1.7.

Machines for the calculation of plait in which the movements connected with positioning and stacking of plait are coordinated and programmed on two or more axes of the main servo positioning and which are specially developed for production of elements of designs of aircraft or rockets from composition materials

8445 40 000;

8445 90 000 1

Technical note.

For the purposes of machine Item 1.2.1.7 for the calculation of plait have capability of the calculation of one threadlike tape or more than width of 25,4 of mm or less, and also tapes and renewals of separate transactions in the course of the calculation are sharp

Technical notes:

1. For the purposes of Item 1.2.1 the main servo positioning (positioning from the main servo-driver) means management of provision of working body (for example, heads) in space by means of the computer program for its exact orientation setting the direction concerning axes of coordinates of the processed detail and achievement of the set requirements of processing.

2. For the purposes of Item 1.2.1 threadlike tape is the continuous strip in the form of the tape executed from the plait or thread fully or partially impregnated with pitch. Fully or partially are impregnated with pitch including the threadlike tapes covered with dry powder which are pasted when heating

1.2.2.

The equipment for production of powders of metal alloys or granular materials having all following characteristics:

a) specially developed for pollution exception; and

b) specially developed for use in one of the processes determined in Item 1.3.2.3.2

1.2.3.

Tools, compression molds, matrixes or armature for morphogenesis in the conditions of superplasticity or diffusion welding of titanium, aluminum or their alloys which are specially developed for production of any of the following:

8207 30 100 0

a) case designs of aircraft or aerospace means;

b) engines for aircraft or aerospace means; or

c) the components which are specially developed for the designs determined in the subitem "an" of Item 1.2. 3, or the engines determined in the subitem "b" of Item 1.2.3

1.3.

Materials

Technical note.

The terms "metals" and "alloys" if other is specially not stipulated, belong to the following raw forms and semifinished products:

a) the raw forms - anodes, blyuma, pigs, briquettes, whetstones, granules, sponge, fraction, cathodes, rings, crystals, bake, procurements of metal of irregular shape, sheets, pellets, tiles, forgings, powders, rods (including the notched rods and procurements for wire), ingots, slabs, glasses, billets, Chushka Spit, spheres;

b) semifinished products (irrespective of, they have cladding, covering, drillings, the punched openings or not):

1) the materials subjected to processing by pressure or different way, received by rolling, drawing, stamping by expression, forging, stamping by shock expression, pressing, granulation, spraying and grinding namely: the disks, products pressed and stamped, rings, films, sheets, plates, forgings, strips, powders, profiles, rods (including uncovered welding rods, additive wire and rod iron), powders, pipes of round and square section, angle-pieces, shaped profiles, foil and thin sheets, scales, channels;

2) the castings received by casting in any forms (sandy, metal, plaster and others), including the procurements and procurements received by methods of powder metallurgy received by casting under pressure, and also baked.

The purpose of control shall not be broken when exporting of the procurements or semifinished products issued for finished products, but, in essence, representing controlled procurements or semifinished products which are not stated above

1.3.1.

The materials which are specially developed for absorption of electromagnetic radiation or the polymers having own conductivity:

1.3.1.1.

Materials for absorption of electromagnetic waves in the field of frequencies from 2 x 108 Hz to 3 x 1012 Hz

3815 19;

3910 00 000 2;

3910 00 000 8

Notes:

1. Item 1.3.1.1 is not applied:

a) to the absorbers of felt type made of natural and synthetic fibers, containing non-magnetic filler;

b) to the absorbers which do not have magnetic losses which working surface is not flat, including pyramids, cones, wedges and spiral-shaped surfaces;

c) to the flat absorbers having all following characteristics:

1) made of any following materials:

the made foam polymeric materials (flexible or nonflexible) with carbon filling or organic materials, including binding, the providing more than 5 percent of reflection in comparison with metal with the wave band, different from average frequency of the falling energy more than for 15 percent, and incapable to maintain temperatures exceeding 450 K (177 °C); or

the ceramic materials providing more than 20 percent of reflection in comparison with metal with the wave band different from average frequency of the falling energy more than for 15 percent, and not capable to maintain temperatures exceeding 800 K (527 °C)

Technical note.

For the purposes of the subitem 1 of the Item "in" notes 1 to Item 1.3.1.1 samples for carrying out testing for absorption shall have the square form with the party at least five lengths of waves of average frequency and be located in distant zone of the radiating element;

2) durability in case of stretching less than 7 x 106 N/sq.m; and

3) durability in case of compression less than 14 x 106 N/sq.m;

d) to the flat absorbers made of the baked ferrite and having all following characteristics:

specific weight of more 4,4 of g/cm3; and

maximum working temperature 548 K (275 °C) or less;

e) to the flat absorbers (absorbers) which do not have magnetic losses, made of expanded plastics with density of 0,15 of g/cm3 or less

Technical note.

Expanded plastics are called the elastic porous materials having the airfilled internal structure. Expanded plastics are also mesh foam materials.

2. The magnetic materials for ensuring absorption of waves specified in the note 1 to Item 1.3.1. 1, are not exempted from control if they contain in paints

1.3.1.2.

The materials opaque to visible light and specially developed for absorption of the near infrared (NIR) radiations having wavelength from more than 810 nanometers to less than 2000 nanometers (frequencies more than 150 TGts, but less than 370 TGts)

3815 19;

3910 00 000 2;

3910 00 000 8

Note.

Item 1.3.1.2 is not applied to materials, specially developed or certain to application in laser marking or welding of polymers;

1.3.1.3.

Electroconductive polymeric materials with volume conductivity it is higher than 10 000 Cm/m (Siemens/m) or 2, with a superficial specific resistance less than 100 Ohms/m received on the basis of any of the following polymers:

1.3.1.3.1.

Polianilina;

3909 39 000 0

1.3.1.3.2.

Polipirrola;

3911 20 000 0

1.3.1.3.3.

Polythiophene;

3911 20 000 0

1.3.1.3.4.

Polyphenylene-vinylene; or

3911 20 000 0

1.3.1.3.5.

Politiyenilen-vinilena

3919 90 000 0

Technical note.

Volume conductivity and superficial specific resistance shall be determined according to standard technique of ASTM D-257 or its national equivalent

Note.

Item 1.3.1.3 is not applied to materials in the liquid state

Special note.

Concerning the materials specified in Items 1.3.1 - 1.3.1.3.5, cm also Items 1.3.1 - 1.3.1.3.5 Sections 2 and 3

1.3.2.

Metal alloys, powders of metal alloys and the alloyed materials of the following types:

1.3.2.1.

Aluminides:

1.3.2.1.1.

The nickel aluminides containing from 15 to 38 percent (on weight) aluminum and at least one additional doping element;

7502 20 000 9

1.3.2.1.2.

The titanium aluminides containing 10 percent (on weight) or more aluminum and at least one additional doping element;

8108 20 000

8108 90 300 8;

8108 90 500 8;

8108 90 600 2;

8108 90 600 7;

8108 90 900 8;

9021 10 800 4;

9021 29 000 4

1.3.2.2.

The metal alloys which are stated below, made of powders or particles of the materials determined in Item 1.3.2.3:

1.3.2.2.1.

Nickel alloys with:

7502 20 000 9

a) resource of long durability of 10000 hours or more at voltage of 676 MPas and temperature 923 K (650 °C); or

b) low-cyclic fatigue of 10000 cycles or more at temperature of 823 K (550 °C) and the maximum tension of cycle of 1095 MPas;

1.3.2.2.2.

Niobic alloys with:

8112 49 000 0;

8112 92 410 0;

8112 99 400 0

a) resource of long durability of 10 000 hours or more at voltage of 400 MPas and temperature 1073 K (800 °C); or

b) low-cyclic fatigue of 10000 cycles or more at temperature of 973 K (700 °C) and the maximum tension of cycle of 700 MPas;

1.3.2.2.3.

Titanic alloys with:

8108 20 000;

8108 90 300 8;

8108 90 500 8;

8108 90 600 2;

8108 90 600 7;

8108 90 900 8;

9021 10 800 4;

9021 29 000 4

a) resource of long durability of 10000 hours or more at voltage of 200 MPas and temperature 723 K (450 °C); or

b) low-cyclic fatigue of 10 000 cycles or more at temperature of 723 K (450 °C) and the maximum tension of cycle of 400 MPas;

1.3.2.2.4.

Aluminum alloys with strength in case of stretching:

7601 20;

7604 29 100 9;

7608 20 810 8;

7608 20 890 7

a) 240 MPas or are higher at temperature of 473 K (200 °C); or

b) 415 MPas or are higher at temperature of 298 K (25 °C);

1.3.2.2.5.

Magnesian alloys:

8104

a) with strength in case of stretching of 345 MPas or above; and

b) with the corrosion speed in 3 percent water solution of sodium chloride less than 1 mm a year measured according to standard technique of ASTM G-31 or its national equivalent;

1.3.2.3.

The powders of metal alloys or particle of material having everything the following characteristics:

1.3.2.3.1.

Made of any following on structure of systems:

Technical note.

X further corresponds to one or more doping elements

1.3.2.3.1.1.

Nickel alloys (Ni-Al-X, Ni-X-Al), for details or components of gas turbine engines, the containing less than three nonmetallic particles more than 100 microns in size (entered in production process) on 109 particles of alloy;

7504 00 000 9

1.3.2.3.1.2.

Niobic alloys (Nb-Al-X or Nb-X-Al, Nb-Si-X or Nb-X-Si, Nb-Ti-X or Nb-X-Ti);

8112 41 000 9;

8112 92 410 0

1.3.2.3.1.3.

Titanic alloys (Ti-Al-X or Ti-X-Al);

8108 20 000 5

1.3.2.3.1.4.

Aluminum alloys (Al-Mg-X or Al-X-Mg, Al-Zn-X or Al-X-Zn, Al-Fe-X or Al-X-Fe); or

7603

1.3.2.3.1.5.

Magnesian alloys (Mg-Al-X or Mg-X-Al); and

8104 30 000 0

1.3.2.3.2.

Made in the controlled circle with use of one of the following processes:

a) vacuum spraying;

b) gas spraying;

c) centrifugal spraying;

d) high-speed tempering of drop;

e) spinningovaniye of fusion and subsequent crushing;

e) extraction of fusion and subsequent crushing;

g) mechanical alloying; or

h) plasma spraying; and

1.3.2.3.3.

Able to be initial materials for receipt of the alloys determined in Item 1.3.2.1 or 1.3.2.2;

1.3.2.4.

The alloyed materials which are characterized by all following:

7504 00 000;

7505 12 000 9;

7506 20 000;

7603 20 000 0;

7604 29 100 9;

7606 12 920 8;

7606 92 000 0;

7607 19;

8104 30 000 0;

8104 90 000 0;

8108 20 000 5;

8108 90 300 8

8108 90 500 8

8112 92 410 0

8112 99 400 0

a) are made of any systems determined in Item 1.3.2.3.1;

b) have the form of not crushed scales, tape or thin cores; and

c) are made in the controlled circle by any of the following methods:

high-speed tempering of drop;

fusion spinningovaniye; or

fusion extraction

Note.

Item 1.3.2 is not applied to metal alloys, powders of metal alloys and the alloyed materials which compounding is specially developed for drawing coverings

Technical notes:

1. To the metal alloys specified in Item 1.3. 2, alloys which contain bigger percent (on weight) the specified metal, than any other elements belong.

2. The resource of long durability should be measured according to standard technique of ASTM E-139 or its national equivalent. 3. The low-cyclic fatigue should be measured according to standard technique of ASTM E-606 "Technical recommendations about testing for low-cyclic fatigue with permanent amplitude" or its national equivalent. Samples shall be loaded in the axial direction with an average of loading indicator, equal unit, and the coefficient of concentration of tension (Kt) equal to unit. The average value of loading is determined as private from division of difference of the maximum and minimum loads of maximum demand.

3. Vacuum spraying - process of spraying of stream of the melted metal on drops with a diameter of 500 microns or less as a result of bystry release of the gas dissolved in metal in vacuum.

4. Gas spraying - process of spraying of stream of the melted metal alloy on drops with a diameter of 500 microns or less in gas stream of high pressure.

5. Centrifugal spraying - process of transformation of stream or the melted metal which is in bathtub by means of centrifugal force in drops with a diameter of 500 microns or less.

6. High-speed tempering of drop - process of bystry hardening of the melted metal hitting against the cooled obstacle with formation of flocculent product.

7. Spinningovaniye of fusion - process of bystry hardening of the stream of the melted metal falling on the rotating cooled drum creating product in the form of wire, tape or scales.

8. Crushing - process of receipt of particles of material (powder) by means of crushing or grinding.

9. Fusion extraction - process of bystry hardening of alloy and extraction of product in the form of tape by means of introduction of short segment of the rotating cooled disk in bathtub with the melted metal alloy.

10. Mechanical alloying - the alloy preparation process consisting in formation of chemical bonds, destruction, gap and formation of the same bonds between powders of net components and powders of master alloys by mechanical impact. Nonmetallic particles by addition of the corresponding powders also can be entered into alloy.

11. Plasma spraying - process of spraying of stream of the melted metal on drops with a diameter of 500 microns or less with use of plasmatrons in the environment of inert gas.

12. Bystry hardening - process in which hardening of fusion of material happens at the speeds of chilling exceeding 1000 Fps

1.3.3.

Magnetic metal materials of all types and in any form, having any of the following characteristics:

1.3.3.1.

Initial relative magnetic permeability 120000 or more and thickness of 0,05 of mm or less

8505 11 000 0;

8505 19 100 0;

8505 19 900 0;

Technical note.

Measurement of initial relative magnetic permeability should be taken on completely annealed materials;

1.3.3.2.

The magnetostrictive alloys having any of the following characteristics:

2846 90 100 0;

2846 90 200 0;

2846 90 300 0;

2846 90 900 0

a) saturation magnetostriction more than 5 x 10-4; or

b) coefficient of magnetomechanical communication (k) of more 0,8; or

1.3.3.3.

The tapes from amorphous or nanocrystal alloys having everything the following characteristics:

7226 11 000 0;

7506;

8105

a) content of iron, cobalt or nickel at least 75 percent (on weight);

b) magnetic induction of saturation (Bs) of 1,6 of T or more; and

c) any of following:

thickness of the film 0,02 of mm or less; or

specific electric resistance 2 x 10-4 Ohms · cm or more

Technical note.

To the nanocrystal materials specified in Item 1.3.3. 3, the materials having the size of crystal grains of 50 nanometers or less determined by method of x-ray diffraction belong

1.3.4.

Urano-titanovye the alloys or tungsten alloys with matrix on the basis of iron, nickel or copper having everything the following characteristics:

2844 10 900 0;

8101 94 000 0;

8101 96 000 0;

8101 99 100 0;

8101 99 900 0;

8108 20 000;

8108 90 300 8;

8108 90 600 2;

8108 90 600 7;

8108 90 900 8;

9021 10 800 4;

9021 29 000 4

a) density is higher than g/cm3 17,5;

b) the limit of elasticity is higher than 880 MPas;

c) strength in case of stretching is higher than 1270 MPas; and

d) relative lengthening more than 8 percent

1.3.5.

The following superconducting conductors from composition materials more than 100 m long or the weight exceeding 100 g:

1.3.5.1.

The conductors from superconducting composition materials containing one or several niobium-titanium threads having all following:

8544

a) laid in matrix not from copper or not on the basis of copper; and

b) 28 x 10-4 mm2 having cross-sectional area less 0, (6 microns in the diameter for threads of round section);

1.3.5.2.

The conductors from superconducting composition materials containing one or several superconducting threads executed not from niobiytitan, having all following:

8544

a) the critical temperature in case of zero magnetic field exceeding 9,85 K (-°C 263,31); and

b) remaining in superconducting condition at 4,2 K temperature (-°C 268,96) in the magnetic field oriented in any directions, perpendicular longitudinal axis of the conductor and corresponding to magnetic induction of 12 T, in case of transmission of electric current with a critical density more than 1750 And/mm2 on all section of the conductor;

1.3.5.3.

The conductors from superconducting composition materials containing one or several superconducting threads remaining in superconducting condition at temperature over 115 K (-°C 158,16)

8544

Technical note.

For the purposes of Item 1.3.5 of thread can be in the form of wire, the cylinder, film, tape or strip

1.3.6.

Liquids and lubricants:

1.3.6.1.

The lubricants containing in quality of the main components the fenilenovy or alkilfenilenovy ethers or monothioesters or their mixes containing more than two radio or thioradio functional groups or their mixes

2909 30 900;

2930 80 000 0;

2930 90 950

1.3.6.1.1 - 1.3.6.1.2.

Are excluded

1.3.6.2.

The damping or floatation liquids answering to everything following:

2903 76 900 0;

3904 69 200 0;

3904 69 800 0

a) having purity of more 99,8 of percent;

b) the containing less than 25 particles of 200 microns in size or more on 100 ml; and

c) received at least for 85 percent from any of the following:

dibromotetrafluoroethane (CAS 25497-30-7, CAS 124-73-2, CAS 27336-23-8);

polychlorotrifluoroethylene (only oily and waxy modifications); or

polibromtriftoretilena;

1.3.6.3.

The fluorocarbon liquids developed for chilling of electronics and having everything the following characteristics:

2903 77 600 0;

2903 77 900 0;

3824 99 960 8

a) the containing 85 percent (on weight) or more any of the following substances or any of their mixes:

monomeric forms of perftorpolialkilefirtriazin or perfluoroaliphatic ethers;

perfluoroalkylamines;

perfluorocycloalkanes; or

perfluoroalkanes;

b) density of 1,5 of g/ml or more at temperature of 298 K (25 °C);

c) liquid state at temperature of 273 K (0 °C); and

d) the containing 60 percent (on weight) or more fluorine

Note.

Item 1.3.6.3 is not applied to the materials determined and packed as medical products

1.3.7.

Ceramic powders, composition materials with ceramic matrix and the corresponding precursors:

1.3.7.1.

Ceramic powders from titanium diboride (TiB 2) (CAS 12045-63-5) having totally metal impurities excepting special additives, less than 5000 parts per million, in case of the average size of particle equal or is less than 5 microns, and at the same time no more than 10 percent of particles have the size more than 10 microns;

2850 00 900 0

1.3.7.2.

Composition materials with ceramic matrix:

1.3.7.2.1.

Composition ceramics ceramics materials with the oxidic or glass matrixes strengthened by any of the following:

a) continuous fibers of any of the following systems: AL2O3 (CAS 1344-28-1); or

Si-C-N; or

2849;

2850 00;

8807 90 000 2;

8807 90 000 3;

8807 90 000 9;

9306 90

Note.

The subitem "an" of Item 1.3.7.2.1 is not applied to the composition materials reinforced by the specified fibers from these systems having strength in case of stretching it is lower than 700 MPas at temperature of 1273 K (1000 °C) or creep deformation more than 1 percent at voltage of 100 MPas and temperature 1273 K (1000 °C) for 100 h

b) the fibers having all following characteristics:

are made of any following materials:

Si-N;

Si-C;

Si-Al-O-N; or

Si-O-N; and

have the specific durability in case of stretching exceeding 12, 7 x 103 m;

1.3.7.2.2.

Composition ceramics ceramics materials with continuous metal phase or without it, the including particles, filamentary crystals or fibers in which the matrix is formed of carbides or silicon nitrides, zirconium or boron

2849 20 000 0;

2849 90 100 0;

2850 00 200 0;

8113 00 200 0;

8113 00 900 0

Special note.

Concerning the materials determined in Item 1.3.7. 2, see also Items 1.3.2 - 1.3.2.2 Sections 2;

1.3.7.3.

The following materials predecessors which are specially developed for production of the materials determined in Item 1.3.7.3:

a) polydiorganosilicon hydrides;

b) polysilazanes;

c) polikarbosilazana

3910 00 000 2;

3910 00 000 8

Technical note.

For the purposes of Item 1.3.7 materials predecessors are the polymeric or metalloorganic materials of specialized appointment used for production of silicon carbide, silicon nitride and ceramics with silicon, carbon or nitric components;

1.3.8.

Not fluorinated polymeric substances:

1.3.8.1.

Following fusible imides in liquid or firm form, including in the form of pitches, powders, granules, films, sheets, films or strips:

1.3.8.1.1.

Bismaleimida;

2925 19 950 0

1.3.8.1.2.

Aromatic polyamide-imides (PAI) having temperature of transition to vitreous condition (Tg) it is higher than 563 K (290 °C);

3908 90 000 0

1.3.8.1.3.

The aromatic polyimide having temperature of transition to vitreous condition (Tg) it is higher than 505 K (232 °C);

3911 20 000 0

1.3.8.1.4.

The aromatic polyetherimides having temperature of transition to vitreous condition (Tg) it is higher than 563 K (290 °C)

3907 29 900 9;

3907 91 900 0

Special note.

For not fusible aromatic polyimide in the form of film, leaf, tape or strip see Item 1.1.3;

1.3.8.2.

Poliarilenovy ketones;

3907 99

1.3.8.3.

Poliarilenovy sulfides where the arilenovy group represents бифенилен, isochrysene or their combinations;

3911 90 190 0

1.3.8.4.

Polibifenilenefirsulfona, having temperature of transition to vitreous condition (Tg) it is higher than 563 K (290 °C)

3911 90 190 0

Technical notes:

1. Temperature of transition to vitreous condition (Tg) for the thermoplastic materials specified in Item 1.3.8.1. 2, and the materials specified in Items 1.3.8.1.4 and 1.3.8. 4, it is determined with use of the method described in the international standard ISO 11357-2(1999) or its national equivalent.

2. Temperature of transition to vitreous condition (Tg) for the thermoreactive materials and materials determined in Items 1.3.8.1.2 and 1.3.8.1.3 respectively is determined with use of method of the three-point bend described in the international standard ASTM D 7028-07 or its national equivalent. Testing shall be carried out on dry sample which reached at least 90 percent of extent of hardening in case of standard thermoreactive processes with the maximum temperature of transition to vitreous condition as it is determined in the ASTM E 2160-04 standard or its national equivalent

1.3.9.

The raw fluorinated connections:

1.3.9.1.

The fluorinated polyimide containing 10 percent (on weight) or more connected fluorine;

3904 69 800 0

1.3.9.2.

The fluorinated fosfazenovy elastomers containing 30 percent (on weight) or more connected fluorine

3904 69 200 0;

3904 69 800 0

1.3.10.

Fibrous or threadlike materials:

Technical notes:

1. For the purposes of calculation of specific durability in case of stretching, the specific module of elasticity or specific weight of the fibrous or threadlike materials determined in Items 1.3.10. 1, 1.3.10.2, 1.3.10.3 or Item 2 of the subitem "an" of Item 1.3.10. 5, their values shall be determined with use of the Method A described in the international standard ISO 10618 (2004) or its national equivalent.

2. Assessment of specific durability in case of stretching, the specific module of elasticity or specific weight of the fibrous or threadlike materials determined in Item 1.3. 10, shall be based on mechanical properties of the unidirectional monofibres containing in them before their conversion in not unidirectional fibrous or threadlike materials

1.3.10.1.

The organic fibrous or threadlike materials having everything the following characteristics:

5402 11 000 0;

5404 12 000 0;

5404 19 000 0;

5501 11 000 0

a) specific module of elasticity more 12, 7 x 106 m; and

b) specific durability in case of stretching more 23, 5 x 104 m

Note.

Item 1.3.10.1 is not applied to polyethylene;

1.3.10.2.

The carbon fibrous or threadlike materials having everything the following characteristics:

6815 13 000 0;

6815 12 000 0

a) specific module of elasticity more 14, 65 x 106 m; and

b) specific durability in case of stretching more 26, 82 x 104 m

Note.

Item 1.3.10.2 is not applied:

a) to the elements of designs from fibrous or threadlike materials of volume or layered structure for repair of civil aircraft having all following:

the area which is not exceeding 1 sq.m;

length which is not exceeding m 2,5; and

width more than 15 mm;

b) to mechanically shtapelirovanny, valyany or cut (lumpy) carbon fibrous or threadlike materials 25 mm long or less;

1.3.10.3.

The inorganic fibrous or threadlike materials having everything the following characteristics:

8101 96 000 0;

8101 99 900 0;

8108 90 300 8;

8108 90 900 8;

9021 10 800 4;

9021 29 000 4

a) corresponding to any of the following:

the specific module of elasticity exceeding 2, 54 x 106 m consisting of 50 percent or more on the weight of silicon dioxide and having; or

having other what the chemical composition and the specific module of elasticity exceeding 5, 6 x 106 m is specified in the paragraph the second this subitem; and

b) the melting point, softenings, decomposition or sublimations in the inert circle exceeding temperature 1922 K (1649 °C)

Note.

Item 1.3.10.3 is not applied:

a) to the discrete, multiphase, polycrystalline fibers of aluminum oxide in the form of the chopped fibers or fibers disorderly laid in mats which are containing 3 percent or more (on weight) silicon dioxide and having the specific module of elasticity less than 10 x 106 m;

b) to molybdenic fibers and fibers from molybdenic alloys;

c) to boron fibers;

d) to discrete ceramic fibers with temperature of melting, softening, decomposition or sublimation in the inert circle it is lower than 2043 K (1770 °C)

1.3.10.4.

The fibrous or threadlike materials having any of the following structures:

1.3.10.4.1.

Consisting of any of the following materials:

1.3.10.4.1.1.

The polyetherimides determined in Item 1.3.8.1.4; or

5402 11 000 0;

5402 20 000;

5402 49 000 0;

5404 12 000 0;

5404 19 000 0;

5501 11 000 0;

5501 20 000 0;

5501 90 000 0;

5503 20 000 0;

5503 90 000 0

1.3.10.4.1.2.

The materials determined in Items 1.3.8.3 and 1.3.8.4; or

5402 20 000;

5402 49 000 0;

5404 12 000 0;

5404 19 000 0;

5501 20 000 0;

5501 90 000 0;

5503 20 000 0;

5503 90 000 0

1.3.10.4.2.

Consisting of the materials determined in Item 1.3.10.4.1.1 or 1.3.10.4.1. 2, and connected with fibers of other types determined in Item 1.3.10. 1, 1.3.10.2 or 1.3.10.3

Technical note.

The connected fibers - consisting from the thermoplastic and reinforcing fibers connected among themselves fiber procurement in which fibers of the first type are matrix precursor;

Special note.

Concerning the materials specified in Items 1.3.10.3 - 1.3.10.4.2, cm also Items 1.3.3 - 1.3.3.2.2 Sections 2;

1.3.10.5.

The fibrous or threadlike materials fully or partially impregnated with pitch or pitch (preprega), the fibrous or threadlike materials covered with metal or carbon (preform) or the carbon fibrous preforms having everything following:

3801;

3926 90 970 6;

6815 13 000 0;

6815 99 000;

7019 11 000 0;

7019 12 000 0;

7019 19;

7019 51 000 0;

7019 61 000 0;

7019 63 000 0;

7019 64 000 0;

7019 65 000 1;

7019 65 000 9;

7019 66 000 1;

7019 66 000 9;

7019 90 002 1;

7019 90 002 9

a) having any of the following:

1) the inorganic fibrous or threadlike materials determined in Item 1.3.10.3; or

2) the organic or carbon fibrous or threadlike materials having everything following:

the specific module of elasticity exceeding 10, 15 x 106 m; and

the specific durability in case of stretching exceeding 17, 7 x 104 m; and

b) having any of the following:

Pitch or baked 1), determined in Item 1.3.8 or 1.3.9.2; or

2) temperature of transition to vitreous condition on dynamic - the thermomechanical analysis (DMA Tg), equal 453 K (180 °C) or above, and also phenol aldehydic polymer; or

3) temperature of transition to vitreous condition on dynamic - the thermomechanical analysis (DMA Tg), equal 505 K (232 °C) or above, and also pitch or baked, not determined in Item 1.3.8 or 1.3.9. 2, and not being fenolo-aldehydic polymer

Technical notes:

1. Carbon fibrous preforms - it is arranged the uncovered or covered fibers located forming product framework which then is filled with matrix therefore composition material is created.

2. Temperature of transition to vitreous condition on dynamic (in time) - to the thermomechanical (granulometric) analysis (DMA Tg) for the materials determined in Item 1.3.10. 5, it is determined with use of the method described in ASTM D 7028-07 or its national equivalent on dry test piece.

For thermoreactive materials extent of hardening of dry test piece shall be at least 90 percent as it is determined by the ASTM E 2160-04 standard or its national equivalent

Notes:

1. The fibrous or threadlike materials covered with metal or carbon (preform) or the carbon fibrous preforms which are not impregnated with pitch or pitch are determined as fibrous or threadlike materials by Item 1.3.10. 1, 1.3.10.2 or 1.3.10.3.

2. Item 1.3.10.5 is not applied:

a) to elements of designs of volume or layered structure from the carbon fibrous or threadlike materials impregnated with matrix from epoxy (prepreg), for repair of civil aircraft, having all following:

the area which is not exceeding 1 sq.m;

length which is not exceeding m 2,5; and

width more than 15 mm;

b) to mechanically shtapelirovanny, valyany or cut (lumpy) carbon fibrous or threadlike materials 25 mm long or less, fully or partially impregnated with pitches or pitches, excellent from determined in Items 1.3.8 or 1.3.9.2

1.3.11.

Following metals and connections:

1.3.11.1.

Metals in the form of particles with sizes less than 60 microns of spherical, powdered, spheroidal forms, scaly or crushed, made of the material containing 99 percent or more zirconium, magnesium or their alloys

8104 30 000 0;

8109 21 000 0;

8109 29 000 0

Technical note.

In case of determination of content of zirconium it joins natural impurity of hafnium (usually 2 - 7 percent)

Note.

The metals or alloys determined in Item 1.3.11. 1, are subject to control irrespective of, they are encapsulated or not in aluminum, magnesium, zirconium or beryllium;

1.3.11.2.

The boron or its alloys which are stated below with particle sizes of 60 microns or less:

2804 50 100 0;

2849 90 100 0

a) boron purity of 85 percent on weight or above;

b) boron alloys with content of boron of 85 percent on weight or above

Note.

The metals or alloys determined in Item 1.3.11. 2, are subject to control irrespective of, they are encapsulated or not in aluminum, magnesium, zirconium or beryllium;

1.3.11.3.

Guanidine nitrate (CAS 506-93-4);

2925 29 000 0

1.3.11.4.

Nitroguanidine (NQ) (CAS 556-88-7)

2925 29 000 0

1.3.12.

Following materials:

1.3.12.1.

Plutonium in any form with plutonium-238 isotope content more than 50 percent (on weight)

2844 20 510 0;

2844 20 590 0;

2844 20 990 0

Note.

Item 1.3.12.1 is not applied:

a) to the deliveries containing plutonium in number of 1 g or less;

b) to the deliveries containing three effective grams of plutonium or less when using as sensitive element in devices;

Technical note.

The effective gram for isotope of plutonium is determined as isotope weight in grams;

1.3.12.2.

Previously enriched neptunium-237 in any form

2844 43 000 0

Note.

Item 1.3.12.2 is not applied to the deliveries containing neptunium-237 in number of 1 g or less

Technical notes:

1. Previously enriched - received using any process for the purpose of increase in concentration of controlled isotope.

2. The materials specified in Item 1.3. 12, are usually used for nuclear sources of heat

Special note.

Concerning the materials specified in Items 1.3.12 - 1.3.12.2, cm also Items 1.3.4 - 1.3.4.2 Sections 2 and Items 1.3.2 - 1.3.2.2 Sections 3

1.4.

Software

1.4.1.

The software, specially developed or modified for development, production or use of the equipment determined in Item 1.2

1.4.2.

The software for development of composition materials with volume or layered structure on the basis of organic, metal or carbon matrixes

Special note.

Concerning the software specified in Item 1.4. 2, see also Item 1.4.1 of Section 2

1.4.3.

The software, specially developed or modified to give the chance to equipments/systems to perform functions of the equipments/systems determined in Item 1.1.4.3 or 1.1.4.4;

1.5.

Technology

1.5.1.

Technologies according to the general technological note for development or production of designs from the composition materials determined in Item 1.1. 2, products from the aromatic polyimide determined in Item 1.1. 3, equipments, systems and component parts determined in Item 1.1. 4, the bullet-proof vests and components determined in Item 1.1. 5, the equipment determined in Item 1.1.6. 2, 1.1.7 or 1.2, or the materials determined in Item 1.3

Special note.

Concerning the technologies specified in Item 1.5. 1, see also Item 1.5.1 of Sections 2 and 3

1.5.2.

Other following technologies:

1.5.2.1.

Technologies of development or production of polypetrolthiazols or polybenzoxazoles;

1.5.2.2.

Technologies of development or production of the ftorelastomerny connections containing at least one vinylradio monomer;

1.5.2.3.

Technologies of development or production of the following ceramic powders or not composition ceramic materials:

1.5.2.3.1.

The ceramic powders having all following:

a) any of the following compositions:

simple or complex zirconium oxides and complex silicon oxides or aluminum;

simple boron nitrides (with cubic crystal lattice);

simple or complex silicon carbides or boron; or

simple or complex silicon nitrides;

b) total metal impurities, excepting purposely brought additives, in the quantity which is not exceeding:

1000 parts per million for simple oxides or carbides; or

5000 parts per million for difficult connections or simple nitrides; and

c) being any of the following:

1) zirconium dioxide (CAS 1314-23-4) having the average particle size equal or is less than 1 have some, and no more than 10 percent of particles the size exceeding 5 microns; or

2) other ceramic powders having the average particle size equal or is less than 5 microns, and no more than 10 percent of particles more than 10 microns in size;

1.5.2.3.2.

Not composition ceramic materials consisting of the materials determined in Item 1.5.2.3.1

Note.

Item 1.5.2.3.2 is not applied to technologies of abrasive materials;

1.5.2.4.

Technologies of assembly, operation or recovery of the materials determined in Item 1.3.1;

1.5.2.5.

Technologies of recovery of designs from the composition materials of volume or layered structure determined in Item 1.1. 2, or the composition materials determined in Item 1.3.7.3

Note.

Item 1.5.2.6 is not applied to technologies of repair of elements of designs of civil aircraft with use of carbon fibrous or threadlike materials and epoxies containing in managements of the producer of aircraft

Special note.

Concerning the technologies specified in Items 1.5.2.5 and 1.5.2. 6, see also Items 1.5.2.1 and 1.5.2.2 of Section 2;

1.5.2.6.

Libraries (parametrical technical databases), specially developed or modified to give the chance to equipments/systems to perform functions of the equipments/systems determined in Item 1.1.4.3 or 1.1.4.4

Category 2. Processing of materials

2.1.

Systems, equipment and components

2.1.1.

Rolling bearings, bearing systems and components:

2.1.1.1.

The ball and one-piece roller radial and radial-stop rolling bearings having everything the admissions determined by the producer according to class of accuracy 4 or 2, or it is better according to the international standard ISO 492 or its national equivalent in which both rings, and bodies of swing are made of copper-nickel alloy or beryllium

8482 10 100 9;

8482 10 900;

8482 30 000 9;

8482 40 000 9;

8482 50 000 9;

8482 91 900 0;

8482 99 000 0

Note.

Item 2.1.1.1 is not applied to conic roller bearings;

Technical notes:

1. Ring - integral part of the radial roller bearing with one or several paths of swing (ISO 5593:1997).

2. Swing body - the ball or roller moving on swing paths (ISO 5593:1997);

2.1.1.2.

The active magnetic bearing systems corresponding to any of the following characteristics, and components which are specially developed for them:

8483 30 380 9;

8483 30 800 7;

8505 11 000 0;

8505 19 100 0;

8505 19 900 0;

8505 90 200 9;

8505 90 900 0

a) are made of material with magnetic induction of 2 T or more and limit of flowability over 414 MPas;

b) are completely electromagnetic with three-dimensional unipolar podmagnichivaniye of the drive; or

c) have high-temperature, with temperature of 450 K (177 °C) and above, position sensors

2.2.

Test, control and production equipment

Technical notes:

1. Secondary parallel axes for planimetric processing (for example, W-axis on horizontally boring machines or secondary axis of rotation which central line is parallel to primary axis of rotation) are not set off in total quantity of axes. The rotation axis optionally means rotation on corner, bigger 360 degrees. Rotation can be set by the device of linear movement (for example, the screw or gear lath).

2. For the purposes of Item 2.2 the quantity of axes which can be jointly coordinated for planimetric management is quantity of axes on which or around which in processing of procurement the simultaneous and interconnected movements between the processed detail and the tool are performed. It does not include any additional axes on which or around which other relative movements in the machine are performed. Such axes include:

a) axes of systems of editing of grinding wheels in grinders;

b) the parallel axes of rotation intended for installation of the separate processed details;

c) the collinear axes of rotation intended for manipulation by one processed detail by its fixing in the boss since the different ends.

3. The nomenclature of axes is determined according to the international standard ISO 841:2001 "Systems of industrial automation and integration. Numerical control by machines. Systems of coordinates and designation of movements".

4. For the purposes of this category the shaking spindle is considered as rotation axis.

5. The declared unidirectional repeatability of positioning for each model of the machine can be used for all machines of one model as alternative to testing of separate machines and is determined by the following:

a) five machines of the model which is subject to assessment are chosen;

b) repeatability is measured (R, R) linear axes according to the international standard ISO 230-2:2014 is also estimated the unidirectional repeatability of positioning for each axis of each of five machines of the chosen model;

c) the arithmetic average value of the unidirectional repeatability of positioning on the basis of measure values of the unidirectional accuracy of positioning for each similar axis of all five machines of the chosen model is determined.

These arithmetic averages of size of the unidirectional repeatability of positioning () become the declared size for each axis of specific model (...) machine;

d) as each of the machines specified in category 2 presents of the Section has several linear axes, the number of the declared sizes of the unidirectional repeatability of positioning of their indicator of accuracy shall be equal to quantity of these linear axes;

e) if any of axes of any model of the machine which is not determined in Items 2.2.1.1 - 2.2.1.3, has the declared unidirectional repeatability of positioning equal or less (better) than certain unidirectional repeatability of positioning of each model of the machine plus 0,7 of micron, then the producer shall confirm again each 18 months positioning accuracy size.

6. For the purposes of Item 2.2 it is not necessary to consider the error of measurement of the unidirectional repeatability of positioning of machines determined according to the international standard ISO 230-2:2014 or its national equivalent.

7. For the purposes of Item 2.2 measurements of axes shall be taken according to the techniques of testing described in Item 5.3.2 of the international standard ISO 230-2:2014. For axes more than 2 m long of testing more than 2 m shall be carried out on pieces. Axes more than 4 m long require several testing (for example, two testing for axes from more than 4 m to 8 m long and three testing for axes from more than 8 m to 12 m long). Each testing shall be carried out with the pieces more than 2 m long which are regularly distributed on axis length. The tested pieces regularly are distributed along the complete length of axis with any excesses of length which are regularly divided at the beginning in the middle of and at the end of the tested piece. The value of all tested pieces specified in the report is the smallest unidirectional repeatability of positioning.

2.2.1.

The machines determined below and any their combinations for processing or cutting of metals, ceramics and composition materials which according to specifications of the manufacturer can be equipped with electronic devices for numerical control:

Notes:

1. Item 2.2.1 is not applied to machines, limited production of cogwheels. For such machines see Item 2.2.3.

2. Item 2.2.1 is not applied to special machines, limited production of any of the following products:

a) cranked or camshafts;

b) the cutting tools;

c) worms of extruders;

d) the engraved or facetted parts of pieces of jewelry; or

e) dentures.

3. The machine having at least two opportunities from three: turning, millings or polishing (for example, the lathe with possibility of milling), it shall be estimated on each corresponding Item 2.2.1. 1, 2.2.1.2 or 2.2.1.3.

4. The machines having function of the additive production in addition to turning, milling or grinding functions shall be estimated on compliance to each of applicable Items 2.2.1. 1, 2.2.1.2 or 2.2.1.3

Special note.

For machines of fair processing (finishing machines) of optics see Item 2.2.2

2.2.1.1.

Lathes with two or more axes which can be jointly coordinated for planimetric management, having any of the following characteristics:

a) the unidirectional repeatability of positioning along one linear axis or more, equal 0,9 of micron or less (better), with the working area less than 1 m; or

b) the unidirectional repeatability of positioning along one linear axis or more, equal 1,1 of micron or less (better), with the working area of 1 m or more

8458;

8464 90 000 0;

8465 20 000 0;

8465 99 000 0

Notes:

1. Item 2.2.1.1 is not applied to the lathes which are specially developed for production of contact lenses and having all following:

a) the controller of the machine is limited to the software with partially programmable data entry, used in the ophthalmologic purposes;

b) lack of the vacuum boss.

2. Item 2.2.1.1 is not applied to prutkovy lathes (turning multi-purpose machines of longitudinal turning) which are intended for processing of the details arriving only through prutkovy feeder have the maximum diameter of rod of 42 mm or less and on which it is impossible to establish holders. Machines can have possibility of drilling or milling for the processed details with a diameter less than 42 mm;

2.2.1.2.

The milling machines having any of the following characteristics:

8459 31 000 0;

8459 51 000 0;

8459 61;

8464 90 000 0;

8465 20 000 0;

8465 92 000 0