DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
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2017-09-18 | 8413302008 | PUMP CONTROLLER HP-90 - PCS 1, IND â„– 10111718014. INTENDED FOR FUEL ENGINE COMBUSTION CHAMBER The Civil Aviation PS-90A AIRCRAFT TYPE IL-76; HIGH PRESSURE FUEL SUPPLY TO CONTROL SYSTEMS mechanization hydraulic cylinders COMP 2. H | *** | RUSSIA | 75 | 29801,02 | *** | ***** | ***** |
2017-09-25 | 8413302008 | PUMP CONTROLLER HP-90 - PCS 1, IND â„– 10111515041. INTENDED FOR FUEL ENGINE COMBUSTION CHAMBER The Civil Aviation PS-90A AIRCRAFT TYPE IL-76; HIGH PRESSURE FUEL SUPPLY TO CONTROL SYSTEMS mechanization hydraulic cylinders COMP 2. H | *** | RUSSIA | 75 | 30000,91 | *** | ***** | ***** |
2017-10-03 | 8413302008 | PUMP CONTROLLER HP-90 - PCS 1, IND â„– 10105616014. INTENDED FOR FUEL ENGINE COMBUSTION CHAMBER The Civil Aviation PS-90A AIRCRAFT TYPE IL-76; The fuel supply to the cylinders HIGH PRESSURE CONTROL SYSTEMS mechanization COMP | ABSENT | RUSSIA | 75 | 29400,81 | PERMIAN | ***** | ***** |
2017-10-03 | 8413302008 | PUMP CONTROLLER HP-90 - PCS 1, IND â„– 10105616014. INTENDED FOR FUEL ENGINE COMBUSTION CHAMBER The Civil Aviation PS-90A AIRCRAFT TYPE IL-76; The fuel supply to the cylinders HIGH PRESSURE CONTROL SYSTEMS mechanization COMP | ABSENT | RUSSIA | 75 | 29400,81 | PERMIAN | ***** | ***** |
2017-10-09 | 8413302008 | PUMP CONTROLLER FUEL WITHOUT FLOWMETER, MARK HP-40TA, IS PART ENGINE turboprop MARKS GTD-350, power 294 kW, ZAV.â„– ENGINE 491 612 018, for civil aircraft (Mi-2); It was in operation, DISTRIBUTED | ABSENT | POLAND | 9 | 1792,21 | YANGON | ***** | ***** |
2017-10-09 | 8413302008 | PUMP CONTROLLER FUEL WITHOUT FLOWMETER, MARK HP-40TA, IS PART ENGINE turboprop MARKS GTD-350, power 294 kW, ZAV.â„– ENGINE 491 612 018, for civil aircraft (Mi-2); It was in operation, DISTRIBUTED | ABSENT | POLAND | 9 | 1792,21 | YANGON | ***** | ***** |