| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-04 | 9014202009 | INERTIAL NAVIGATION SYSTEM :: PART.â„– HG2030BE03 - ELECTRONIC CONTROL UNIT INERTIAL inertial navigation system designed to determine the spatial location of use. AT civilian passenger B / C TYPE A320, serial | *** | RUSSIA | 7.2 | 287794,86 | *** | ***** | ***** |
| 2017-09-08 | 9014208009 | Barometric Altimeter, B / N 64141-362-1, b / y, the arrow, the diaphragm, diaphragm type, is used to measure the relative flight altitude of the sun, DOES NOT CONTAIN radio electronic facilities and high frequency devices, aeronautical, removed from the Civil passage: PC | *** | RUSSIA | 0.45 | 500 | *** | ***** | ***** |
| 2017-09-11 | 9014202009 | INERTIAL NAVIGATION SYSTEM, NOT MILITARY: PART.â„– HG2030AE23 - ELECTRONIC CONTROL UNIT INERTIAL (ADIRU) inertial navigation system B / C. It designed to determine the spatial location of the plane, AIR PARAM | *** | RUSSIA | 7.8 | 316193,7 | *** | ***** | ***** |
| 2017-09-22 | 9014800000 | INTEGRATED DEVICE ELECTRONIC RESERVE. Are components of avionics systems ITS FUNCTIONS processing and display FLIGHT INFORMATION attitude indicator, altimeter, speed of flight. USTANAVLIVAVETSYA: Sun DRY civilian passenger RRJ95: MODEL R | *** | RUSSIA | 3.68 | 141257,18 | *** | ***** | ***** |
| 2017-09-23 | 9014208009 | Inertial unit air data unit is an electronic module consisting of electronic circuit boards, logic circuits and electric sockets. SUPPLY VOLTAGE 115 V and 28 V supply is used to transmit and receive navigation signals REQUIRED | *** | RUSSIA | 7.8 | 170108,51 | *** | ***** | ***** |
| 2017-09-24 | 9014208009 | POSITION INDICATOR rudder trim Amphibious A319 / A320 / A321 CIVIL AVIATION: P / N 196PN01Y02, LABELING 125-43910344 NOT SCRAP ELECTRIC OR ELECTRICAL COMPONENTS, NOT MILITARY NOT APPLY TO electronic means and VYSOKOCH | *** | RUSSIA | 0.19 | 725,9 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-10-10 | 9014208009 | SENSOR vertical acceleration (accelerometer) B / N 223-00107-196 - 1pc., P / N 9034 (B / V, fault), electronic-mechanical device consists of a housing, a sensor with a sensing element and electric sockets, IS NOT RADIOELECTRONIC : Supplementary Accessories | *** | RUSSIA | 0.17 | 24767,2 | *** | ***** | ***** |
| 2017-10-10 | 9014208009 | Apparatus and instruments for air navigation for civil aircraft AN-26B-100, CIVIL USE, NOT yavl. Electronic means and V / H device in a state of disrepair for repair: UNITED STATES OF LIGHT VERTICAL | *** | RUSSIA | 2.3 | 18177,11 | *** | ***** | ***** |
| 2017-10-10 | 9014900000 | CONTROL UNIT IS ELECTRONIC DISTRIBUTION BLOCK and outputting command signals to the actuator control fly MODE autopilot, it is a part of AP-34B autopilot SERIES 2 CIVIL MI-8 CONTROL UNIT F | *** | RUSSIA | 6.3 | 3500 | *** | ***** | ***** |