| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-04 | 9026208000 | Elektrotermometriia (RECEIVER AND INDEX) EDMU-6; (0-6) KG / PCS SM2-20, new pressure sensors designed for monitoring the fluid pressure in the fuel supply system, lubrication and cooling of internal combustion engines, no electronic obshchegrazhdanskogo: Dest. | *** | RUSSIA | 14 | 2720,87 | *** | ***** | ***** |
| 2017-09-05 | 9026900000 | Indicators of fuel H / H 01/01/2101, b / y, PART CONTROL SYSTEM amount of fuel, is designed to monitor the amount of fuel in the tank and display the value of digitally WHEN ADDING Sun installed in the fuel system, the sun, radioactive: FIRST | *** | RUSSIA | 0.25 | 500 | *** | ***** | ***** |
| 2017-09-05 | 9026900000 | EXPANSION B / N 391041-027, B / V. ELECTRICAL PART MEASUREMENT AND INDICATORS FUEL CONSUMPTION. IS A sensor for measuring the amount of fuel in the central fuel tank on board aircraft. RADIOACTIVE SOURCE NONE, removed from the CET: AN | *** | RUSSIA | 0.3 | 500 | *** | ***** | ***** |
| 2017-09-05 | 9026208000 | PRESSURE SENSOR with electrical output signal. INTENDED FOR THE CONTROL OF PRESSURE FUEL DIESEL EXCAVATOR KOMATSU PC400LC-7 (absolute pressure). ARTICLE ND499000-6141 PRESSURE FUEL - 1 PCS. NOT | *** | RUSSIA | 0.45 | 371,67 | *** | ***** | ***** |
| 2017-09-06 | 9026108100 | SENSOR FUEL, removed from the previously imported and released into free circulation CIVIL passenger aircraft CESSNA 208B BORT.â„–RA-67422. PURPOSE: DESIGNED FOR MEASURING FUEL CONSUMPTION BY PLANE CESSNA-208B. CONSTRUCTION: IS MET | *** | RUSSIA | 0.33 | 1500 | *** | ***** | ***** |
| 2017-09-06 | 9026208000 | Pressure Switch, is a sensor for at elevated pressure in fuel system aircraft. DOES NOT CONTAIN sources of ionizing radiation. Radioactive sources are absent. IS SET FOR THE PASSENGER ALARM PRESSURE CAM | *** | RUSSIA | 0.4 | 3295,96 | *** | ***** | ***** |
| 2017-09-07 | 9026108100 | Fuel gauge (B / D), DO NOT FLOAT NOT VORTEX, vane type. Radioactive sources does not. Consists of a metal enclosure, inside which the impeller (BLADE). P / N 9-127-83 - 2 PCS, S / N AC1481, ZZ141.. On the case there P | *** | RUSSIA | 1.2 | 8802,49 | *** | ***** | ***** |
| 2017-09-07 | 9026900000 | Indicators of fuel H / H 02/01/2101, b / y, PART CONTROL SYSTEM amount of fuel, is designed to display the value of digitally WHEN ADDING BC, sets FUEL on board the aircraft, radioactive sources missing, C: OD | *** | RUSSIA | 0.25 | 500 | *** | ***** | ***** |
| 2017-09-08 | 9026900000 | Needle indicator TEMPERATURE AND PRESSURE FUEL / OIL B / H LUN 1538.01-8, C / H BA0002, BA0001-2SHT. (ANSERVIS., D / Y) pointer with dial and scale YAVL.CHASTYU PRESSURE FUEL CONTROL SYSTEM Before entering the ENGINE range of 0 to 0.39 MPa (0 - 4 | *** | RUSSIA | 0.54 | 40 | *** | ***** | ***** |
| 2017-09-08 | 9026208000 | GAUGE PRESSURE FUEL B / H LUN 1559-8, C / H UC0044, AB0076-2SHT. (ANSERVISNYE, B / Y) SENSOR ELEKTROMEHANICH.TIPA, PREDN.DLYA PREOBRAZOV.DAVLENIYA FUEL LINE ENGINE PROPORTS.ELEKTRICH.SIGNAL and transfer it for display on the instrument in the cockpit, BNW | *** | RUSSIA | 0.44 | 50,01 | *** | ***** | ***** |