| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-05 | 9014202009 | Gyro horizon AGB-3K (2010 GV) INERTIAL NAVIGATION SYSTEM FOR DETERMINATION OF HELICOPTER in space relative to the true horizon of the plane, the error of indication of the instrument, measured on a scale pitch and SCALE ROLL ON AND ZERO: UHL | *** | RUSSIA | 4.22 | 7251,9 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-10-11 | 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 | 0.7 | 588,55 | *** | ***** | ***** |
| 2017-10-17 | 9014202009 | INERTIAL NAVIGATION SYSTEM, NOT MILITARY. FOR CIVIL AVIATION. NAVIGATION inertial unit AHRS. HOW IT WORKS: generate data about the aircraft position in the emergency mode. The unit is integrated ACCELEROMETER (sensor measurements ACCEL | *** | RUSSIA | 2.37 | 29587,68 | *** | ***** | ***** |
| 2017-10-17 | 9014202009 | Gyro horizon AGB-3K (2012 GV) INERTIAL NAVIGATION SYSTEM FOR DETERMINATION OF HELICOPTER in space relative to the true horizon of the plane, the error of indication of the instrument, measured on a scale pitch and SCALE ROLL ON AND ZERO: UHL | *** | RUSSIA | 4.22 | 7882,83 | *** | ***** | ***** |