| 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 | 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 | *** | ***** | ***** |
| 2017-09-05 | 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 | *** | ***** | ***** |
| 2017-09-13 | 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 | *** | ***** | ***** |
| 2017-09-23 | 9014900000 | ATTACK ANGLE SENSOR (FLUGER) H / H 861CAS3, B / C. PART NAVIGATION SYSTEM Sun INSTALLED ON side of the fuselage and is intended for the Sun Provisions Sun control in the pitch channel and signaling about approaching the critical angles of attack (stall). Removal from: GRAZH | *** | RUSSIA | 1.25 | 1916,44 | *** | ***** | ***** |
| 2017-09-25 | 9014900000 | GAUGE AOA W / H C16258AB, b / y, (part of the navigation equipment) to determine the angle between the center line of aircraft and the horizon, transmits the received data to the PC PROTECTION stall, DOES NOT CONTAIN electronic means and You | *** | RUSSIA | 0.9 | 1560 | *** | ***** | ***** |
| 2017-09-25 | 9014900000 | Giroagregata W / H 060-0015-00 NAVIGATION SYSTEM FOR DETERMINING yaw (exchange) and angular rotation about the vertical axis HELICOPTER AND DATA TRANSMISSION IN INDICATOR cockpit, removed from civilian helicopter AS355NP RA-07240, AS: 35 | *** | RUSSIA | 3.89 | 24202,3 | *** | ***** | ***** |
| 2017-09-26 | 9014900000 | PART onboard navigating system of civil helicopters Mi-8 MTV-1, not for military purposes. SENSOR roll rate. APPLICATION: PART AVPOPILOTA AP-34. Mounting Kit: OUTLET OS2RMD24BPN10G5V1 2 pcs. The angular velocity sensor pitch. | *** | RUSSIA | 14.8 | 42080 | *** | ***** | ***** |
| 2017-09-27 | 9014900000 | Inertial unit B / H HG1050AE10, B / Y, IS PART OF THE NAVIGATION SYSTEM Sun, Use to measurement and calculation of linear acceleration and angular velocity about the axes TURN roll, pitch, and yaw AIRCRAFT CONTAINS 3 laser gyro and 3: AKC | *** | RUSSIA | 17.95 | 591,3 | *** | ***** | ***** |