DATE | HS_CODE | Product Description | Trademark | Country | Net Weight | Statistical Cost | Place | Shipper Name | Consignee Name |
---|
2017-09-01 | 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 | *** | UNITED STATES | 1.74 | 10707,65 | *** | ***** | ***** |
2017-09-06 | 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 | *** | UNITED STATES | 1.71 | 10574,81 | *** | ***** | ***** |
2017-09-06 | 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 | *** | UNITED STATES | 1.7 | 7146,65 | *** | ***** | ***** |
2017-09-20 | 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 | *** | UNITED STATES | 1.73 | 4745,81 | *** | ***** | ***** |
2017-11-14 | 9014202009 | Gyro horizon AGB-96D (2009 GV): INERTIAL NAVIGATION SYSTEM, used to establish the helicopter in space relative to the true horizon of the plane, the error of indication of the instrument at zero ANGLES AND TOWN 0-30. Of +/- 1 | TEMP-AVIA | RUSSIA | 2.5 | 7825,55 | Bang | ***** | ***** |
2017-11-22 | 9014202009 | Artificial horizon B / N AGB-96D INERTIAL NAVIGATION SYSTEM, used to establish the helicopter in space relative to the true horizon of the plane, the error of indication of the instrument at zero ANGLES AND TOWN 0-30. Of +/- 1 degree. ON | TEMP-AVIA | *** | 2.5 | 500 | TYUMEN | ***** | ***** |
2017-11-28 | 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 | ABSENT | FRANCE | 1.72 | 8317,02 | HOFDDORF | ***** | ***** |
2017-11-30 | 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 | ABSENT | *** | 3.5 | 11017,7 | Stansted | ***** | ***** |