DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-08-02 | 2710192100 | FUEL FOR turbojet TYPE kerosene JET A-1, -PROTSENT DISTILLATION OIL TEMPERATURE 210 ° C (ISO METHOD 3405, equivalent method ASTM D86) of less than 90% -PROTSENT ON DISTILLATION OIL TEMPERATURE 250 ° C:. (P | *** | RUSSIA | 26000000 | 13208114,77 | *** | ***** | ***** |
2017-08-09 | 2710192100 | FUEL FOR turbojet TYPE kerosene JET A-1, -PROTSENT DISTILLATION OIL TEMPERATURE 210 ° C (ISO METHOD 3405, equivalent method ASTM D86) of less than 90% -PROTSENT ON DISTILLATION OIL TEMPERATURE 250 ° C:. (P | *** | RUSSIA | 13000000 | 6467514,25 | *** | ***** | ***** |
2017-08-11 | 2710192100 | FUEL FOR turbojet TYPE kerosene JET A-1, -PROTSENT DISTILLATION OIL TEMPERATURE 210 ° C (ISO METHOD 3405, equivalent method ASTM D86) of less than 90% -PROTSENT ON DISTILLATION OIL TEMPERATURE 250 ° C:. (P | *** | RUSSIA | 7000000 | 3517488,75 | *** | ***** | ***** |
2017-08-15 | 2710192100 | FUEL FOR turbojet TYPE kerosene JET A-1, -PROTSENT DISTILLATION OIL TEMPERATURE 210 ° C (ISO METHOD 3405, equivalent method ASTM D86) 74,5 vol.% -PROTSENT DISTILLATION OIL TEMPERATURE 250 ° C (PO : IU | *** | RUSSIA | 12334801 | 5739023,77 | *** | ***** | ***** |
2017-08-17 | 2710192100 | FUEL FOR turbojet TYPE kerosene JET A-1, -PROTSENT DISTILLATION OIL TEMPERATURE 210 ° C (ISO METHOD 3405, equivalent method ASTM D86) of less than 90% -PROTSENT ON DISTILLATION OIL TEMPERATURE 250 ° C:. (P | *** | RUSSIA | 42000000 | 20726874,85 | *** | ***** | ***** |
2017-09-04 | 8411910008 | Parts of turbojets: 338-067-014-0 PART.â„– - Titanium vane guide rib inner stillness plenum OF POWER PLANTS turbojet (engine) aircraft. Use. AT civilian passenger B / C TYPE A3 | *** | RUSSIA | 1.4 | 6698,09 | *** | ***** | ***** |
2017-09-04 | 8411910008 | Parts of turbojets: 338-067-014-0 PART.â„– - Titanium vane guide rib inner stillness plenum OF POWER PLANTS turbojet (engine) aircraft. Use. AT civilian passenger B / C TYPE A3 | *** | RUSSIA | 1.75 | 6698,09 | *** | ***** | ***** |
2017-09-04 | 8411910008 | Parts of the turbojet engine for maintenance civil passenger aircraft in order to maintain their summer FITNESS. BLADE FAN MOTOR. Fan blades first-stage engine low-pressure compressor. get up | *** | RUSSIA | 32 | 262061,94 | *** | ***** | ***** |
2017-09-05 | 9032810000 | Instruments and devices, hydraulic or pneumatic, NOT MILITARY: PART.â„– 66503-8061-536 - HYDROMECHANICAL unit automatically control the fuel delivery in a turbojet. Use. AT civilian passenger B / C TYPE A321 WOODW | *** | RUSSIA | 29 | 201852,66 | *** | ***** | ***** |
2017-09-05 | 9032810000 | Instruments and devices, hydraulic or pneumatic, NOT MILITARY: PART.â„– 66503-8061-535 - HYDROMECHANICAL unit automatically control the fuel delivery in a turbojet B / C. MAINTENANCE AND (OR) REPAIR CET | *** | RUSSIA | 28.8 | 341612,28 | *** | ***** | ***** |