| 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 | *** | ***** | ***** |
| 2017-09-05 | 9014900000 | PART trawl PROBES FOR SHIPS CIVIL FLEET - UNIT UNIT TRALOVY TRALOVY designed to convert electrical pulses in the echo signal and vice versa, operating frequencies, 50kHz, ACCURACY OVER 200M +/- 1.5%, NAPRYAZH.220V, power less than 90VA, IN DEPTH | *** | RUSSIA | 8 | 5155,97 | *** | ***** | ***** |
| 2017-09-08 | 9014900000 | CONTROL UNIT autopilot B / H S12850BS02 (2002G.V.) INCLUDED IN THE SYSTEM COMPOSITION AFC (PART AUTOPILOT), designed to provide an interface between the crew and the automatic control system SM. ANNEX flight P: AB | *** | RUSSIA | 5.31 | 3000 | *** | ***** | ***** |
| 2017-09-11 | 9014800000 | Strapdown inertial navigation system (identification number 16018), designed to determine navigation parameters COMMERCIAL MOVING OBJECTS TO PARTICIPATE IN TESTING FOR RELIABILITY AND PRECISION: NPK "OPTOLIN | *** | RUSSIA | 5.7 | 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 | *** | ***** | ***** |
| 2017-09-12 | 9014900000 | UNIT gyroscopic GA-8: 1991 GV, PART NAVIGATION SYSTEM COMB-2 is designed for averaging and memorizing COURSE HELICOPTER, to work as POLUKOMPASA, for outputting signals COURSES Planning and navigational instruments and equipment. In SC | *** | RUSSIA | 3.6 | 2223,54 | *** | ***** | ***** |
| 2017-09-15 | 9014208009 | ULTRASONIC BEACON UNIT RECORDS OF NEGOTIATIONS crew members. It is not part of recording unit: Designed for applying the ultrasonic signal to the detection unit records of negotiations CREW when falling the sun on the water surface. LIGHTHOUSE FULFILLED in aluminum | *** | RUSSIA | 0.39 | 1560 | *** | ***** | ***** |
| 2017-09-19 | 9014900000 | KAT. 13.2 OF NAVIGATION SYSTEMS MODULE inertial sensors (ISM) CEP. Number 00289, for warranty OF CONTRACT (CONSTRUCTION), IS part of the laser inertial navigation system designed for use in combination | *** | RUSSIA | 7.95 | 158530,7 | *** | ***** | ***** |
| 2017-09-20 | 9014208009 | Turnout, barometric altimeter. Party. â„– 4016341-905. DEFECTIVE, removed from civilian passenger sun BOMBARDIER DHC-8-311 (Q300), BOARD. â„– VQ-BVJ. : Designed for visual display of the current pressure altitude flight (HEIGHT computing | *** | RUSSIA | 1.1 | 2013,59 | *** | ***** | ***** |
| 2017-09-25 | 9014800000 | Attitude indicator is designed for installation on a civilian Mi-17-1B. INTENDED FOR detecting and indicating the spatial position of the helicopter on the roll and pitch. INSTALLED on the dashboard. Not for military purposes. NOT ON SCRAP artificial horizon | *** | RUSSIA | 2.5 | 42515,13 | *** | ***** | ***** |