| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 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 | *** | ***** | ***** |
| 2017-09-13 | 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 | *** | ***** | ***** |
| 2017-09-23 | 9014202009 | BLOCK inertial reference system Amphibious A319 / A320 CIVIL AVIATION: 125-43910311 MARKING is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to transverse, longitudinal | *** | RUSSIA | 11.3 | 6800,31 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-26 | 9014208009 | Apparatus and instruments for air navigation, NOT MILITARY ,: PART.â„– 17A717-03-00 - LINE AKSELEROMETER - devices measure acceleration in three axes AIRCRAFT. POWER accelerated action pendulum mechanism that produces electrical CIGNA | *** | RUSSIA | 0.4 | 6197,04 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-28 | 9014202009 | BLOCK inertial reference system for the aircraft AIRBUS A319 / A320 / A321 civil aviation. : 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 to the longitudinal axis | *** | RUSSIA | 12.18 | 30093,35 | *** | ***** | ***** |
| 2017-10-01 | 9014202009 | BLOCK inertial reference system Amphibious A319 / 320 CIVIL AVIATION: LABELING 125-43910473. It is used to determine the aircraft's position by calculating the angular coefficient and linear acceleration at an inclination of the aircraft relative to transverse, longitudinal | *** | RUSSIA | 7.73 | 64591,96 | *** | ***** | ***** |