| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-01 | 9014900000 | UNIT OF DYNAMIC MEASUREMENT DATA (UDMU) is a sensor AUTOPILOT UAV and measure the angles of pitch and roll, the dynamic pressure 1pc. ITEM Used. Not a hazardous waste. :: RADA: OUTPOST AD677601-01: RADA 1 | *** | *** | 1.03 | 36458,71 | *** | ***** | ***** |
| 2017-09-04 | 9014800000 | The angular velocity sensor SX-WR-03.PREDNAZNACHEN FOR USE IN DETERMINING ORIENTATION small spacecraft. METER IS BASED angular velocity sensor element, taken along the MEMS Technology. ENGINEERING MO | *** | RUSSIA | 0.4 | 8420 | *** | ***** | ***** |
| 2017-09-04 | 9014900000 | Inertial unit B / H HG1050AD11, B / Y, IS PART OF THE AIRCRAFT NAVIGATION SYSTEM serves for the measurement and calculation of linear acceleration and angular velocity about the axes TURN roll, pitch, and yaw, AIRCRAFT, CONTAINS 3 laser gyro: And | *** | RUSSIA | 18.7 | 594,25 | *** | ***** | ***** |
| 2017-09-04 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes pitch of 45 degrees: B | *** | RUSSIA | 1.77 | 500 | *** | ***** | ***** |
| 2017-09-05 | 9014900000 | Trawl PROBES OF VESSELS FOR CIVIL flotation SENSOR CORES trawl SIS-SENSOR 50 CORES trawl 50 SIS-TECHNICAL WORKING frequency-50 +/- 1 KHz, the maximum operating depth-1000M, RANGE COMMUNICATION IN WATER-TO 500M, POWER SENSOR | *** | RUSSIA | 3.1 | 1873,83 | *** | ***** | ***** |
| 2017-09-09 | 9014800000 | Apparatus and instruments for air navigation or space navigation (excluding compasses): Multipurpose devices (CHART PLOTTER) with integrated GPS receiver for positioning on the ground, built-in portable antenna, power supply range 2.4-5 V, not | *** | RUSSIA | 11.36 | 14149,32 | *** | ***** | ***** |
| 2017-09-13 | 9014900000 | Inertial unit B / H 465020-04000402, B / Y, IS PART OF THE AIRCRAFT inertial systems, is used to measure and calculation of linear acceleration and angular velocity about the axes TURN roll, pitch, and yaw AIRCRAFT CONTAINS 3 gyroscopes and 3 A | *** | RUSSIA | 11.1 | 3000 | *** | ***** | ***** |
| 2017-09-13 | 9014900000 | Inertial unit B / H 465020-03030316, B / Y, IS PART OF THE AIRCRAFT inertial systems, is used to measure and calculation of linear acceleration and angular velocity about the axes TURN roll, pitch, and yaw AIRCRAFT CONTAINS 3 gyroscopes and 3 A | *** | RUSSIA | 11.5 | 3000 | *** | ***** | ***** |
| 2017-09-14 | 9014202009 | BLOCK inertial reference system for aircraft A319 / A320 / A321 CIVIL AVIATION: LABELING 020-6327 3140 is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to the transverse | *** | RUSSIA | 7 | 186000 | *** | ***** | ***** |
| 2017-09-15 | 9014208009 | Nautical instruments: AOA SENSOR P / N C16291AB, the angle between the fuselage and the AXIS BUILDING VECTOR AIR FLOW FOR VS-320/321/319, goods / used. : THALES AVIONICS SAS THALES AVIONICS SAS C16291AB 0 | *** | RUSSIA | 1.8 | 1446,23 | *** | ***** | ***** |