| DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
|---|
| 2017-09-04 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes pitch of 45 degrees: B | *** | RUSSIA | 1.77 | 500 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-09-28 | 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 | *** | ***** | ***** |
| 2017-10-03 | 9014202009 | INERTIAL NAVIGATION SYSTEM FOR THOSE. SERVICE INTERNATIONAL COURTS CET. TRANSPORTATION. BLOCK inertial navigation system. It is arranged to calculate the aircraft's position AT ANY TIME. The block consists of 3 X-laser gyroscope, 3- | *** | RUSSIA | 18.6 | 500 | *** | ***** | ***** |
| 2017-10-11 | 9014202009 | RESERVE artificial horizon NAVIGATION SYSTEM W / N 501-1657-02, b / y, inertial gyroscopic, is designed to determine the spatial position of the sun relative to the plane the true horizon are installed in the cockpit, DOES NOT CONTAIN THE SAKE: MA | *** | RUSSIA | 1.3 | 588,55 | *** | ***** | ***** |
| 2017-10-12 | 9014202009 | Artificial horizon B / H H341ANM1, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE axes of pitch 45 °: OB | *** | RUSSIA | 1.9 | 500 | *** | ***** | ***** |
| 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 | *** | ***** | ***** |
| 2017-10-20 | 9014202009 | Artificial horizon B / H H341ANM1, CER.â„– 7590, b / y, RESERVE (INERTIAL NAVIGATION SYSTEM) inertial, turnouts, mechanical, gyroscopic, for detecting and indicating the plane's position, compensation ANGLE TO AXIS PITCH: A | *** | RUSSIA | 1.75 | 500 | *** | ***** | ***** |