| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-03 | 8414592000 | (3302.1308060) axial fan 11 blades, with viscous clutch assembly, the diameter of 410 mm, POWER CONSUMPTION - 4.6 ITC FOR OPERATION IN THE COOLED ENGINE FOR A / M MARKS Gazelle, Gazelle "NEXT", Gazelle BUSINESS civil use -.: 12 | *** | *** | 19.2 | 597,58 | *** | ***** | ***** |
| 2017-09-03 | 8411910008 | PART turbojet and turboprop engines: 338-002-114-0 PART.â„– - TITANIUM BLADE FAN POWER turbojet installation, use. AT civilian passenger B / C TYPE 320, identification mark VP-BRZ, SERIAL NUMBER 3157 UNKNOWN unknown | *** | *** | 3.2 | 15983,68 | *** | ***** | ***** |
| 2017-09-04 | 8409910008 | OF MILITARY NOT USED FOR PISTON INTERNAL COMBUSTION ENGINE WITH SPARK IGNITION FOR VEHICLES, AGRICULTURAL MACHINERY: FAN MOTOR 3 X MANUAL. 236-1308011-r2 DRIVE FAN 236NE-1308011-E2 YaMZ absent | *** | RUSSIA | 110 | 628,71 | *** | ***** | ***** |
| 2017-09-04 | 8411121009 | Turbofan engines are (B / D), has a thrust of 41 kN. It consists of the fan, the compressor HIGH PRESSURE combustion chamber high pressure turbine, a low pressure turbine and the nozzle. The flow of hot compressed gas coming from as a result of | *** | RUSSIA | 1000 | 155557,51 | *** | ***** | ***** |
| 2017-09-04 | 8411121009 | Turbofan engines are (B / D), has a thrust of 41 kN. It consists of the fan, the compressor HIGH PRESSURE combustion chamber high pressure turbine, a low pressure turbine and the nozzle. The flow of hot compressed gas coming from as a result of | *** | RUSSIA | 1000 | 155850,33 | *** | ***** | ***** |
| 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 | 8414592000 | Spare parts for motorcars, axial fan used in the system air-cooled engine combustion CAR domestic production not intended for industrial assembly: the blower motor ASSEMBLY 8 Lopasov | *** | RUSSIA | 36.26 | 296,61 | *** | ***** | ***** |
| 2017-09-05 | 8481805990 | Fixture, NOT MILITARY: CLASSIFICATION CODE PART.â„– VT0250A04 - Turbofan CONTROL VALVE FOR AIR SUPPLY SYSTEM OF AIR INTAKE ENGINE BC, used on board a civil passenger aircraft A320, S / N AIRCRAFT 2106 About | *** | RUSSIA | 0.6 | 16050,75 | *** | ***** | ***** |
| 2017-09-05 | 8411910008 | PART turbo-jet and turboprop engines, NOT MILITARY: PART.â„– FW29479 - BLADE turbofan first stage low-pressure compressor powered aircraft HA . It is made of titanium alloy. INTENDED FOR AIR INTAKE | *** | RUSSIA | 11.2 | 67153,46 | *** | ***** | ***** |
| 2017-09-05 | 8414592000 | ENGINE COOLING FAN 3302 (10 blades) Cat 03302-0-1308010-010 - 30: ENGINE COOLING FAN 3302 (blade 10). APPLICATION: Automotive, axial fan: ORGPLAST Ltd. Nizhny Novgorod None None 03 | *** | RUSSIA | 25.5 | 53,78 | *** | ***** | ***** |