| 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 | *** | ***** | ***** |
| 2017-09-05 | 9014208009 | ACCELEROMETER B / N 971-4193-001, it is designed to measure linear acceleration (vertical, lateral and longitudinal acceleration) in the flight and runway mode and transmitting information to FDAU block (FLIGHT INFORMATION GATHERING), set I | *** | RUSSIA | 0.8 | 500 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-20 | 9014208009 | Accelerometer, B / N 971-4193-001, is designed to measure linear acceleration in the flight and runway mode and transmitting information to the acquisition unit FLIGHT INFORMATION IN THE ELECTRICAL Sun, radioactive sources missing, SOD: EP | *** | RUSSIA | 0.5 | 599,65 | *** | ***** | ***** |
| 2017-09-21 | 9014202009 | ACCELEROMETER B / H 3001-01-111, b / y, inertial, navigation, are designed to measure linear acceleration (vertical, lateral and longitudinal) in the flight and runway mode and transmitting information to BLOCK FDAU, IS NOT RADIOELEKTR: OH | *** | RUSSIA | 0.6 | 500 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-26 | 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 | *** | ***** | ***** |